Initial Public Offering (IPO): Registration Statement (General Form) — Form S-1
Filing Table of Contents
Document/Exhibit Description Pages Size
1: S-1 @Entertainment, Inc. 185 1.02M
2: EX-2.1 Form of Contribution Agreement 20 57K
3: EX-2.2 Form of Purchase Agreement 10 33K
4: EX-3.1 Amended & Restated Certificate of Incorporation 18 73K
5: EX-3.2 Bylaws of @Entertainment, Inc. 40 174K
6: EX-3.3 Form of Shareholders Agreement 80 230K
7: EX-3.4 Termination Agreement 3 14K
8: EX-3.5 Form of Registration Rights Agreement 23 74K
9: EX-5 Opinion of Baker & McKenzie 2 13K
10: EX-8 Form of Opinion of Baker & McKenzie 1 10K
11: EX-9.1 Form of Voting Agreement 7 26K
12: EX-9.2 Side Letter 5 16K
15: EX-10.11 Employment Agreement 6 37K
16: EX-10.12 Stock Option Agreement 11 54K
17: EX-10.13 Form of Employment Agreement 5 37K
18: EX-10.14 Form of Employment Agreement 6 33K
19: EX-10.15 Stock Option Agreement 11 53K
20: EX-10.16 Form of Stock Option Plan 29 74K
21: EX-10.19 Agreement for Digital Transmission 96 233K
13: EX-10.2 Form of Management Agreement 3 12K
22: EX-10.20 Agreement for Digital Transmission 95 231K
23: EX-10.21 Agreement for Digital Transmission 95 235K
14: EX-10.3 Form of Service Agreement 12 38K
24: EX-11.1 Statement Re: Calculation of Per Share Earnings 1 10K
25: EX-15 Letter From Kpmg Peat Marwick LLP 1 10K
26: EX-21 List of Subsidiaries 1 11K
27: EX-23.1 Consent of Kpmg Peat Marwick LLP 1 11K
28: EX-23.2 Consent of Kpmg Peat Marwick LLP 1 11K
29: EX-27 ƒ Financial Data Schedule 1 11K
Exhibit 10.20
CONFIDENTIAL
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AGREEMENT
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for digital transmission on the ASTRA system
between
SOCIETE EUROPEENNE DES SATELLITES S.A.
PCI PROGRAMMING INC.
CONFIDENTIAL
[Download Table]
1. Interpretation . . . . . . . . . . . . . . . . . . . . . . . 4
2. Agreement . . . . . . . . . . . . . . . . . . . . . . . . . 6
3. Term . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
4. Charges . . . . . . . . . . . . . . . . . . . . . . . . . . 6
5. Spare TWTA . . . . . . . . . . . . . . . . . . . . . . . . . 7
6. Unavailability . . . . . . . . . . . . . . . . . . . . . . . 7
7. Excluding Circumstances . . . . . . . . . . . . . . . . . . 8
8. Interruption Testing and Monitoring . . . . . . . . . . . . 8
9. Pre-emption . . . . . . . . . . . . . . . . . . . . . . . . 9
10. Use of Transponder and Encryption . . . . . . . . . . . . . 9
11. Service Information . . . . . . . . . . . . . . . . . . . . 9
12. Compliance with Law . . . . . . . . . . . . . . . . . . . . 10
13. SES' Authority . . . . . . . . . . . . . . . . . . . . . . . 10
14. Assignment . . . . . . . . . . . . . . . . . . . . . . . . . 10
15. Termination . . . . . . . . . . . . . . . . . . . . . . . . 11
16. Effect of Termination . . . . . . . . . . . . . . . . . . . 11
17. Force Maieure . . . . . . . . . . . . . . . . . . . . . . . 12
18. Limitation of Liability - Exclusivity of Remedies . . . . . 12
19. Indemnities . . . . . . . . . . . . . . . . . . . . . . . . 12
20. Confidentiality . . . . . . . . . . . . . . . . . . . . . . 13
21. Trademark - Logo and Press Releases . . . . . . . . . . . . 13
22. Notices . . . . . . . . . . . . . . . . . . . . . . . . . . 13
23. Severability . . . . . . . . . . . . . . . . . . . . . . . . 13
24. Waiver . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
25. Entire Agreement . . . . . . . . . . . . . . . . . . . . . . 14
26. Amendment . . . . . . . . . . . . . . . . . . . . . . . . . 14
27. Proper Law and Jurisdiction . . . . . . . . . . . . . . . . 14
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CONFIDENTIAL
[Download Table]
28. Legal Opinion . . . . . . . . . . . . . . . . . . . . . . . 14
29. Condition Precedent . . . . . . . . . . . . . . . . . . . . 14
30. Marketing Cooperation . . . . . . . . . . . . . . . . . . . 14
[Download Table]
SCHEDULE I: Satellite and Transponder Description and
Performance Specifications . . . . . . . . . . . . . 16
SCHEDULE II: Customer Signals, Customer Uplink Signals and
Uplink Facilities . . . . . . . . . . . . . . . . . 18
SCHEDULE III: Service(s) . . . . . . . . . . . . . . . . . . . . . 20
SCHEDULE IV: Monitoring . . . . . . . . . . . . . . . . . . . . . 21
SCHEDULE V: Conditional Access system . . . . . . . . . . . . . 23
SCHEDULE VI: Charges . . . . . . . . . . . . . . . . . . . . . . 24
SCHEDULE VII: Priority and Pre-emption . . . . . . . . . . . . . . 26
SCHEDULE VIII: ASTRA Access Agreement . . . . . . . . . . . . . . . 29
SCHEDULE IX: ASIUS . . . . . . . . . . . . . . . . . . . . . . . 30
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CONFIDENTIAL
AGREEMENT
DATED 26 MARCH 1997
BETWEEN:
(1) Societe Europeenne des Satellites S.A. L-6815 Chateau de Betzdorf, Grand
Duchy of Luxembourg ("SES"); and
(2) PCI Programming Inc.
c/o Poland Communications Inc.
1 Commercial Plaza
Hartford, CT 06033, USA (the "Customer")
PREAMBLE:
(A) SES is the operator of the ASTRA satellite system which comprises several
satellites co-located at 19.2 degrees East for the retransmission of
television and radio services;
(B) The satellite, described in Schedule I-A hereto, is part of this
satellite system;
(C) The Customer wishes to use transponder capacity on a transponder of said
satellite to transmit the digital services described herein on the terms
and conditions set out below;
IT IS HEREBY AGREED AS FOLLOWS:
1. INTERPRETATION
1.1 In this Agreement, the following words and expressions shall have
the meanings ascribed to them below:
"Cahier des Charges" : the ministerial enactment (arrete
ministeriel) of the Luxembourg government setting out the duties to
be observed by SES in performance of the Concession;
"Concession" : the concession contract ("Contrat de Concession")
entered into by the government of Luxembourg and SES to enable SES
to operate the Satellite System and any amendment thereof;
"Customer Downlink Signals" : downlink RF(1)-QPSK(2) modulated time
division multiplexed carrier carrying the Service(s) from the
Customer's Transponder;
--------------------------
1. Radio frequency
2. Quadrature phase shift keying
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"Customer Signals": the bit stream, carrying the Service(s),
produced by the Customer and transmitted to the Uplink Facilities
for onward transmission via the Customer's Transponder and
conforming to SCHEDULE II;
"Customer Start Date" or "CSD": the date on which the Customer has
agreed to commence the transmission of the Service(s) on the
Customer's Transponder, being the date upon which the Board of SES
and the Government of Luxembourg have given their approval even if
the Government's approval and operational service date of ASTRA 1G
has occurred;
"Customer Uplink Signals": the RF-QPSK modulated time division
multiplexed carrier, carrying the Service(s), transmitted from the
Uplink Facilities to the Customer's Transponder and conforming to
SCHEDULE II;
"Customer's Transponder": the transponder capacity on the Satellite
as described in SCHEDULE I-B, or any alternative transponder
capacity subsequently allocated to the Customer pursuant hereto, and
via which the Customer transmits the Service(s);
"Expiry Date": the last day of the Term;
"LIBOR": the one month London inter bank offered rate, applying to
the currency of this Agreement, as quoted by Banque et Caisse
d'Epargne de l'Etat in Luxembourg on the due date for payment;
"Minimum Transponder Performance": as defined in SCHEDULE I-D;
"Operational Service Dates" or "OSD": the date on which SES declared
the Satellite operational, being 1 June 1996;
"Payment Period": a period of the Term in respect of which payments
are payable or have been paid pursuant to SCHEDULE VI;
"Pre-emption": the deliberate interruption and/or cessation of the
availability of a transponder by SES in accordance with the rules
set out in SCHEDULE VII and "Pre-empt" shall be construed
accordingly;
"Received Signal Power": as defined in SCHEDULE I-D;
"Satellite": the ASTRA 1F satellite as described in SCHEDULE I-A;
"Service(s)": the Customer's services described in SCHEDULE III;
"SES' Associates": SES' officers, employees, consultants, agents,
contractors or subcontractors however it is understood that CLT/DTS
performing the play-out for the Customer, are not considered as SES
Associate;
"Spare TWTA": a spare travelling wave tube amplifier which can be
switched to recover traffic on the Satellite;
"Target Market": as defined in SCHEDULE III;
"Term": the duration of this Agreement as specified in CLAUSE 3;
"transponder": a part of the Satellite which receives, amplifies and
frequency.
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CONFIDENTIAL
translates the uplink signals and retransmits them as downlink
signals;
"UNAVAILABLE", UNAVAILABILITY": as defined in CLAUSE 6;
"UPLINK FACILITIES": all equipment and ancillary facilities used to
transmit the Customer Uplink Signals to the Satellite conforming to
SCHEDULE II;
"VAT": Value added tax or any similar tax or charge.
1.2 In case of conflict between this Agreement and the Schedules hereto,
this Agreement shall prevail.
2. AGREEMENT
With effect from CSD SES will perform the transmission of the Customer
Uplink Signals carrying the Service(s) by exclusively providing the
Customer's Transponder for the purpose and monitor the digital transmission
of the Customer Uplink Signals on the terms set out herein. This Agreement
does not include multiplexing and uplinking.
3. TERM
3.1 This Agreement shall begin on the date hereof and expire on the
tenth (10th) anniversary of CSD.
3.2 Either party may terminate this Agreement upon 6 months written
notice if the Customer does not target the Polish DTH market prior
to 1 January 1999. "Target the Polish DTH market" means that (i)
the Customer shall have a licence or permit (if necessary) for its
activity and (ii) actively markets and promotes DTH reception by
ensuring availability in the market of decoder boxes (integrated
receiver devices ("IRD's").
3.3 Notwithstanding any other term of this Agreement:
(i) SES may terminate this Agreement immediately by notice in
writing to the Customer if an event of free majeure prevents
the Satellite from becoming operational;
(ii) The Customer may terminate this Agreement by not less than
thirty (30) days prior written notice to SES at any time prior
to 31 December 1998.
In either case, each party shall be discharged of all liability and
obligation to the other.
4. CHARGES
4.1 The Customer shall pay the charges set out in SCHEDULE VI as and on
the dates set out therein.
4.2 Sums overdue shall be subject to a late payment interest charge at
2% over LIBOR from the due date. The interest shall accrue on a
daily basis.
4.3 All sums payable by the Customer under SCHEDULE VI are quoted
exclusive of any VAT or other tax or duties. The Customer
undertakes to pay any applicable VAT, other tax or duties upon
receipt of an appropriate invoice from SES.
4.4 All sums due under this Agreement shall be paid in full without
set-off, counter-claim or other deduction.
4.5 Any sums owed by SES to the Customer for Unavailability pursuant to
CLAUSE 6 shall be calculated by SES within 15 days from the date on
which such an event occurred and shall be paid to the Customer
within thirty (30) days thereafter. If the Customer disagrees with
the amount so calculated and notified by SES, the Customer shall so
notify SES in writing and the parties shall seek in good faith to
resolve the disagreement. Payments for Unavailability after the due
date for
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payment determined hereunder shall accrue interest at the rate set
out in CLAUSE 4.2, unless such payments are in dispute.
4.6 In the circumstances set out in CLAUSE 7.2, the Customer shall not
be relieved of its obligation to pay the charges payable hereunder.
5. SPARE TWTA
If the Customer's Transponder becomes Unavailable and if a spare TWTA is
available, then, subject to the priority rules set out in SCHEDULE VII, SES
shall provide its use to the Customer as soon as reasonably possible.
6. UNAVAILABILITY
6.1 The Customer's Transponder shall be regarded as Unavailable if:
6.1.1. the Received Signal Power falls below the Minimum Transponder
Performance by more than 1 dB;
6.1.2 the interruption of the Service(s) pursuant to CLAUSE 8.1
exceeds thirty (30) minutes in any calendar quarter;
6.1.3 any failure of the Satellite or any part thereof causes an
interruption of transmissions of the Service(s); or
6.1.4 the 27.5 MS/s QPSK digital carrier at the centre frequency of
the Customer's Transponder, complying fully with SCHEDULE II,
which saturates the Customer's Transponder as indicated by
the satellite DLA input power telemetry as specified by SES
and has a 3/4 rate FEC, exhibits a Bit Error Rate worse than
10-9 when received on a typical 60 cm antenna with no
pointing error, with a G/T of no worse than 13.5 dB/K located
in Betzdorf, Luxembourg, under clear sky conditions. It is
understood that SES shall have no obligation to monitor the
bit error rate.
6.2 During any period of Unavailability the Customer may obtain (at its
cost) temporary bridging services from an alternative service
provider. The Customer's payment obligations hereunder shall be
suspended from the start of the period of Unavailability to the end
of such period or, if later, the date the Customer's arrangements
for bridging services in respect of such period of Unavailability
come to an end, however such date shall not be later than 30 days
after the end of any period of Unavailability. In this regard, SES
shall refund to the Customer the pro rata temporis portion of the
charges paid by the Customer for the period of Unavailability and/or
the Customer shall not be liable to pay SES the pro rata temporis
portion of the charges payable (but not yet paid) in respect of such
period of Unavailability (as applicable).
6.3 If the Customer's Transponder becomes Unavailable for a period of
thirty (30) or more consecutive days, then the Customer may
terminate the Agreement by written notice to SES ( provided that
such notice is sent while the Customer's Transponder is Unavailable)
and CLAUSE 16.1 shall apply.
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CONFIDENTIAL
6.4 Clauses 5, 6.2 and 6.3 shall be the Customer's sole remedies in the
event of an Unavailability and SES shall have no other obligation.
7. EXCLUDING CIRCUMSTANCES
Clauses 6.2 and 6.3 shall not apply:
7.1 to an Unavailability caused by an act or omission of the Customer or
of the customer's Associates;
7.2 where the Customer Signals, the Customer Uplink Signals or the
Uplink Facilities do not comply with Schedule II or where the
Customer Signals are not received by the Uplink Facilities or the
Customer Uplink Signals are not received by the Customer's
Transponder due to no fault of SES or any SES Associate.
8. INTERRUPTION, TESTING AND MONITORING
8.1 SES shall be entitled to interrupt the Service(s) and to require the
Customer to cease transmission of the Customer Uplink Signals where
necessary (i) to provide the cause of a Spare TWTA, and (ii) for
operational testing, maintenance, monitoring, preventive or curative
repair or adjustment to be carried out either with respect to the
Satellite as a whole or part thereof, or one or more of its
transponders where necessary, in SES' reasonable opinion, to
preserve the integrity of the Satellite or the overall quality of
the satellite transmissions in the short, medium or long term. SES
shall give the Customer as much notice thereof as is practicable in
the circumstances and shall agree with the Customer upon the date
and time of interruption wherever possible.
8.2 SES shall also be entitled to interrupt the Service(s) or to require
the Customer to cease transmission of the Customer Uplink Signals if
the Customer is in breach of its obligations hereunder ALWAYS
PROVIDED THAT if such breach is due to a technical issue, SES shall
not interrupt the Service(s) without allowing the Customer
reasonable period of time to correct it, unless the technical issue
either (i) is interfering with another customer of SES, (ii) could
cause potentially damage or degradation to the Satellite or to its
proper functioning or (iii) could affect the quality of the
transmissions provided by the Satellite. Nothing in this CLAUSE 8.2
shall permit SES to interrupt the Services in circumstances where
there is a bona fide dispute between the parties as to any fees due
to be paid under this Agreement. Any such dispute, if not resolved
by negotiation, shall be dealt with as provided for in CLAUSE 27.
8.3 SES shall monitor the Customer Uplink Signals and the performance of
the Customer's Transponder in accordance with the provisions of
SCHEDULE IV and supply an analysis of the results when so requested
by the Customer. Such data shall be limited to information which SES
can reasonable be expected to obtain and which it can reveal without
liability or breach of any duty to any third party. Such information
shall be kept confidential.
8.4 The Customer shall procure that the operator of the Uplink
Facilities shall assist SES in making any tests to ensure that such
Facilities and the Customer Uplink
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CONFIDENTIAL
Signals comply with Clause 10.3
8.5 All Service(s) using the Customer's Transponder shall be uplinked
from the same uplink antenna.
9. PRE-EMPTION
- Intentionally deleted -
10. USE OF TRANSPONDER AND ENCRYPTION
10.1 The frequencies for the Customer Uplink Signals and the Customer
Downlink Signals initially allocated by SES shall be those stated in
Schedule 1-B or notified to the Customer before CSD.
10.2 The Customer shall, on CSD, commence transmitting the Service(s) and
thereafter maintain full transmission of the majority of the
Service(s) as described in SCHEDULE III. For the avoidance of doubt
this CLAUSE 10.2 is not designed to interfere with the Customer's
plans for the roll out of the Service(s) and SES accepts that such
plans do not envisage the transmission of a full complement of
Service(s) for the first year of this Agreement and may also mean
that the Customer does not have any Service(s) ready to commence
transmission on CSD.
10.3 The Customer shall procure that the Customer Signals and Customer
Uplink Signals and Uplink Facilities comply with SCHEDULE II and do
not interfere with or damage the Satellite or any of its
transponders.
10.4 The Customer may, if so provided in SCHEDULE V, encrypt the Customer
Signals provided that the Customer, at its costs, provides SES with
ten operational decoders authorised for reception and any other
equipment needed to receive the Customer Downlink Signals.
10.5 SES shall have the right, at any time, to replace the transponder
carrying the Service(s) on the Satellite by another transponder on
any other ASTRA satellite at the same orbital position provided that
the replacement transponder has the same polarization, bandwidth and
the same uplink and downlink signal frequency as the transponder
used by the Customer prior to such replacement and provides Minimum
Transponder Performance. Unless SES uplinks the Service(s), SES will
endeavour to provide to the Customer advance notice of 24 hours to
perform the necessary operations to uplink the Service(s) to the
other ASTRA satellite. To avoid a Service interruption, the Customer
shall take all necessary arrangements with the operator of the
Uplink Facilities to accommodate such a transponder replacement and
SES will either (i) move the Customer's Transponder in tandem with
any other customer's transponder on the Satellite or (ii) relax the
technical requirements of the Access Agreement to require only two
(2) uplinks for the three (3) allocated customer's transponders with
frequencies in the E and F bands.
10.6 The Customer shall not use the Customer's Transponder in any way not
specified in this Agreement.
11. SERVICE INFORMATION
The Customer shall provide to SES the Service(s) information in compliance
with SCHEDULE III.
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CONFIDENTIAL
12. COMPLIANCE WITH LAW
12.1 The Customer shall comply to all material extent with all laws,
regulations or provisions relevant for the performance of this
Agreement, shall, where necessary, at all times have and comply with
a broadcasting license or authorization for the Service(s) and shall
promptly inform SES of any material change thereof. If the
Service(s) is not subject to the laws of a member of the European
Union it shall, nevertheless, comply with the provisions of the
""Television Without Frontiers'' directive of 3 October 1989, as may
be amended, as transposed into the laws of Luxembourg being
currently Article 6 and Chapter IV of the Luxembourg Electronic
Media Law of 27 July 1991.
12.2 SES shall not exercise its right to terminate this Agreement
under CLAUSE 15.1 by reason of non-compliance by the Customer
pursuant to CLAUSE 12.1 except where such non-compliance has been
determined by a court or other authority with competent jurisdiction
or where otherwise requested by the Government of the Grand Duchy of
Luxembourg. Moreover if compliance with CLAUSE 12.1 would result in
the contravention of any future law or regulation in the Target
Market, its non-compliance with CLAUSE 12.1 shall constitute an
event of force majeure.
13. SES' AUTHORITY
This Agreement is subject to the continuing right of SES to provide the
Customer's Transponder pursuant to the Concession and the Cahier des
Charges. If this right is withdrawn, then this Agreement shall terminate
automatically unless the Government of Luxembourg wishes to undertake SES'
rights and obligations hereunder. In either case, SES shall be discharged
of all liability and obligation to the Customer subject to CLAUSE 16.
14. ASSIGNMENT
14.1 Subject to the remainder of this CLAUSE 14 the Customer shall not
assign, transfer, sub-let, or otherwise allow any third party to
directly or indirectly exercise its rights, in whole or in part,
under this Agreement. For the purpose hereof, an assignment shall
also include a change in the control of the Customer or of a
substantial part of its assets or business.
14.2 SES hereby authorises the Customer at any time to assign its rights
under this Agreement to (a) any affiliate or (b) Procable Sp Z O.O.
(""Procable'') provided that the Customer retains not less than a
33% shareholding in Procable, and in any such event on condition
that the Customer agrees to continue to be bound by all its
obligations and liabilities hereunder and to hold SES harmless from
any breach of this Agreement by its Assignee. For the purposes of
this CLAUSE 14.2, a company will be regarded as an affiliate of the
Customer if the Customer holds not less than a 50% interest in the
shares or equivalent of that company or if the company holds at
least 50% interest in the Customer or a company being under common
control with the Customer.
14.3 Upon SES' and the Luxembourg Government prior written consent, which
shall not be unreasonably withheld or delayed, the Customer may
sub-contract the benefit of
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this Agreement to any third party provided that (i) no such
sub-contract shall relieve the Customer of its obligations and
liabilities under this Agreement and the Customer shall be
responsible for the acts, default and omissions of the sub-
contractor, its employees and agents as fully as if they were
acts, default, omissions of the Customer itself and (ii) the
Customer will share revenues exceeding the charge payable in the
relevant calendar year with SES on a 50/50 basis.
15. TERMINATION
In addition to the termination rights provided herein including without
limitation the Customer's right to terminate as specified in CLAUSE 6.3, a
party may terminate this Agreement forthwith by written notice of the other
party:
15.1 commits a material breach of its obligations hereunder and fails to
remedy such breach (if capable of remedy) within thirty (30) days
of written notice from the party requiring such breach to be
remedied (for the avoidance of doubt, circumstances giving rise to
the right to terminate under CLAUSE 3.2 or CLAUSE 6.3 do not
constitute a material breach);
15.2 is unable to pay its debts as they mature; becomes insolvent; is
subject to bankruptcy, reorganisation, moratorium, insolvency or
similar proceedings for the relief of financially distressed
debtors; is subject to winding up, dissolution or liquidation
(judicial or non-judicial) proceedings; voluntarily or involuntarily
suspends or discontinues its business; liquidates or sells a
substantial part of its assets; makes an assignment for the benefit
of its creditors; or is subject to the appointment of a receiver,
liquidator or other third party over its assets or business; or
15.3 has been prevented by an event of force majeure from materially
performing its obligations hereunder for sixty (60) days or more.
SES will waive its right to terminate the Agreement if and for such
period of time the Customer continues to pay the charge hereunder.
16. EFFECT OF TERMINATION
16.1 Where the Agreement is terminated (i) by the Customer, pursuant to
CLAUSES 6.3, 15.1 or 15.2, (ii) by either party, pursuant to CLAUSE
15.3, or (iii) automatically pursuant to CLAUSE 13, then SES shall
refund to the Customer the pro rata temporis portion of the advance
payments made by the Customer pursuant to SCHEDULE VI relating to
the unexpired portion of the Payment Period in progress on the date
of termination. SES may deduct from such amount all payments, taxes
and duties payable to governments or other entities for which the
Customer is liable hereunder and all sums owed to SES at that time.
16.2 Where SES terminates this Agreement pursuant to CLAUSES 15.1 or
15.2, the Customer shall forthwith pay to SES any sum owed by the
Customer to SES at that time and shall continue to be liable for and
to pay the charge provided in SCHEDULE VI (as if the Agreement had
not been terminated) until such time as SES allocates the Customer's
Transponder to another customer. SES shall have no obligation to
market the Customer's Transponder in priority to unused transponder
capacity on
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SES' satellites and for a price inferior to that payable by the
Customer to SES (unless the Customer makes up for the difference);
however, SES shall use its reasonable efforts to mitigate ITS
losses. If the Customer's Transponder is allocated to another
customer, SES shall refund to the Customer the pro rata temporis
portion of the advance payments made by the Customer pursuant to
SCHEDULE VI relating to the unexpired portion of the Payment Period
in progress on the date at which the other customer starts
transmitting.
17. FORCE MAJEURE
Neither party shall be considered to be in breach or be liable for any
damage suffered by the other party or its Associates, by reason of any
failure to perform any obligation hereunder if and for so long as such
failure is the result of an event of force majeure. Subject to CLAUSE
15.3, the respective obligations of both parties shall be suspended for
such time as such an event prevents either party from performing its
obligations.
18. LIMITATION OF LIABILITY - EXCLUSIVITY OF REMEDIES
18.1 Without prejudice to CLAUSES 5,6, and 16, SES shall not be
liable to the Customer or to the Customer's Associates in any way
whatsoever, except for its gross negligence ("faute lourde") or
wilful misconduct ("dol").
18.2 The remedies expressly provided in this Agreement are the sole
remedies available to the parties and the parties waive any other
rights that they may have.
19. INDEMNITIES
19.1 The Customer shall totally indemnify SES and SES' Associates and
customers against all claims, losses, damages, expenses arising
from:
19.1.1 damages caused to third parties as a result of a breach by
the Customer of this Agreement or a civil duty;
19.1.2 infringement of copyright, defamation, libel or invasion of
privacy (or any allegation thereof) arising in the course of
the use of the Customer's Transponder;
19.1.3 claims in any way connected with the quality or contents of
any programme or display transmitted as part of the
Service(s), or with any failure, however caused, to perform
an obligation owed to any person to transmit any such
programme or display;
19.1.4 infringement by the Customer by virtue of exercising its
rights under this Agreement of any other third party right;
19.1.5 damage caused to the Satellite by the Customer or the
operator of the Uplink Facilities save where SES is said
operator.
19.2 A party (the "First Party") shall indemnify the other party
against all caims, losses,
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damages or expenses arising from an infringement of patent caused by
the use of any apparatus or system provided by the First Party to
the other.
19.3 Neither party shall admit any liability or make any concession in
respect of any claim brought against it for which it may seek an
indemnity under this CLAUSE 19 without the prior written consent of
the indemnifying party and the indemnifying party shall have the
right to control any such proceedings at its own costs and expenses.
20. CONFIDENTIALITY
Each party shall, and shall procure that its Associates shall, both
throughout the TERM and thereafter, keep confidential the provisions of
this Agreement together with all other information disclosed on a
confidential basis by the other party hereunder and shall not disclose the
same to any person except when acting under a court order. Unless otherwise
specified in writing, all information regarding the performance of the
Satellite or the Customer's Transponder or the business affairs of the
parties shall be regarded as confidential. Where necessary to secure its
financing or otherwise in the legitimate course of its business, each party
shall have the right to disclose this Agreement to its professional
advisors, financial institutions and stock exchanges authorities.
21. TRADEMARK - LOGO AND PRESS RELEASES
21.1 Each party agrees to allow the other to use its trademark and logo,
free of charge, throughout the Term, solely for the purpose of
indicating in any document, advertising or communication made or
commissioned by such party that the Service(s) is transmitted via
the ASTRA satellite system.
21.2 The parties shall agree on a press release to announce this
Agreement.
22. NOTICES
Any notice shall be in writing and shall be sent to the address of the
party to be served as above written or to such other address previously
notified to the other party. All notices shall be delivered by hand,
registered, or certified post or facsimile. Notices shall be deemed to have
been received: (i) if delivered by hand, upon such delivery, (ii) if sent
by post, (seventy-two) 72 hours after the envelope containing such notice
was posted, or (iii) if sent by facsimile, when the transmission of the
facsimile is complete. Notices sent by facsimile shall be confirmed by
letter. The initial facsimile number of the parties are: (i) SES: (352) 710
725 291, (ii) the Customer: (48) 22 43 56 31 or (48) 22 43 65 31.
23. SEVERABILITY
In the event that a provision of this Agreement is held to be invalid,
inapplicable or unenforceable such provision shall be replaced by one which
comes closest to the intention of the parties and the remaining provisions
of this Agreement shall be unimpaired.
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CONFIDENTIAL
24. WAIVER
No relaxation, delay or indulgence by either party in enforcing any right
under this Agreement shall operate as a waiver thereof.
25. ENTIRE AGREEMENT
This Agreement, with the Schedules, is the entire agreement between the
parties in connection with the subject matter hereof and there are no
other agreements, written or oral. This Agreement supersedes all prior
understandings, representations or communications between the parties and
each party declares that it has not relied on any representation except as
expressly set out herein.
26. AMENDMENT
No provision of this Agreement may be amended, waived or terminated, nor
may any breach thereof be waived otherwise than (in each case) by the
express written agreement of the parties hereto. The Agreement will, where
necessary, be amended to reflect the reasonable changes made by the
Luxembourg Government to the Concession or the Cahier des Charges or the
Luxembourg Laws.
27. PROPER LAW AND JURISDICTION
This Agreement shall be governed by and construed in accordance with the
laws of the Grand Duchy of Luxembourg and the parties hereby submit to the
exclusive jurisdiction of the Luxembourg courts.
28. LEGAL OPINION
The Customer shall, at SES' request and cost, procure a legal opinion
issued by the Customer's external counsel in favour of SES' lending
institutions, in a form reasonably satisfactory to SES and its lending
institutions.
29. CONDITION PRECEDENT
This Agreement is subject to (i) the approval of the Board of SES, the
Board of the Customer and of the Government of Luxembourg and (ii) the
availability of the Customer's Transponder at SES. The parties shall each
use their reasonable efforts to obtain the approvals required and SES shall
use its reasonable efforts to make the Customer's Transponder available as
soon as practicable after contract signature but in any event before 30
April 1997.
30. MARKETING COOPERATION
Taking into account the Customer's plan to introduce into the market an
aggregate amount of 500,000 IRD's during the start phase of DTH SES and the
Customer shall cooperate jointly
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CONFIDENTIAL
in the marketing activities for rolling out the Customer's digital
services. Such cooperation shall be mutually agreed from time to time.
IN WITNESS WHEREOF the duly authorised representatives of the parties hereto
have executed this agreement in two originals on the date first before written.
PCI PROGRAMMING INC. SOCIETE EUROPEENNE DES SATELLITES S.A.
------------------- --------------------
By: Romain Bausch
Title: Director General
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SCHEDULE I: SATELLITE AND TRANSPONDER DESCRIPTION AND PERFORMANCE
SPECIFICATIONS
A. ASTRA 1F SATELLITE DESCRIPTION
1. Satellite Manufacturer : Hughes Communications
Int. Inc.
2. Expected Fuel Lifetime (from OSD) : 14 years
3. Satellite Station-keeping accuracy : Longitude +/- 0.10 degrees
Inclination +/- 0.10 degrees
4. Stabilisation System : 3 axis
5. Designed Channel Capacity :
A maximum of 20 transponders at start of life reducing to 20 transponders
at end of life can be operated simultaneously. All transponders are
eclipse protected and may be selected from the following configurations:
18 transponders in the 17300 - 17700 MHz uplink and 11700 - 12100 MHz
downlink frequency band, 16 transponders in the 12750 - 13000 MHz uplink
and 10700 - 10950 MHz downlink frequency band (ASTRA 1D backup), 16
transponders in the 13000 - 13250 MHz uplink and 10950 - 11200 MHz downlink
frequency band (ASTRA 1C backup), 16 transponders in 14000 - 14250 MHz
uplink and 11450 - 11700 MHz downlink frequency band (ASTRA 1B backup).
6. Polarization : Dual Linear
7. Cross-polarization isolation (for areas
within the 50 dBW e.i.r.p. contour) on
vertical and horizontal transponders : Typical 30 dB
For the avoidance of doubt, the specifications set out in Parts B and C
below shall constitute part of the terms and conditions of this Agreement
but the description of the Satellite in this Part A is for the Customer's
information only and shall not constitute any term or condition of this
Agreement.
B. SPECIFIC DESCRIPTION OF TRANSPONDER USE
1. Initial transponder number on the Satellite : 79
2. Customer Uplink Signal frequency : 17592.50 MHz
3. Customer Downlink Signal frequency : 11992.50 MHz
4. Capacity provided : 27.5 MS/s QPSK
5. Hours of transmission : 24 hours per day
6. Pre-emptibility status : See SCHEDULE VII-A
7. Polarisation : Horizontal
C. ORBITAL POSITION AND TRANSPONDER BANDWIDTH
1. Orbital position : 19.2 degrees East
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2. Usable Transponder bandwidth : 33 MHz (in the band 12.10
to 12.50 GHz)
D. TRANSPONDER PERFORMANCE
1. "MINIMUM TRANSPONDER PERFORMANCE" is defined as a satellite single carrier
saturation e.i.r.p. measured under clear sky conditions by a measurement
test set-up according to standard engineering practice as described in
SCHEDULE I-E of:
[Download Table]
F-Band F-band on
City on ASTRA 1F ASTRA 1G
--------- ----------- ---------
Bialystok 50 50
Gdansk 52.5 50.5
Kielce 52 51.5
Krakow 52 52
Lublin 50 51
Olsztyn 52 50.5
Radom 51.5 51.5
Warsaw 51.5 51
Wroclaw 52.5 52
Betzdorf 51 51
It is understood that SES shall have no obligation to monitor or measure
the Minimum Transponder Performance in any sites listed above save for
Betzdorf.
2. "RECEIVED SIGNAL POWER" is defined as signal power in dBW on the ground in
Luxembourg measured by a measurement test set-up according to standard
engineering practice as described in SCHEDULE I-E. If the measurement is
not performed under clear sky conditions, the measured value shall be
corrected to account for the effect of weather and propagation conditions.
3. The Minimum Transponder Performance and Received Signal Power shall be
those measured or otherwise ascertained where the Customer is complying or
procuring compliance with SCHEDULE II.
E. MEASUREMENT TEST SET-UP AND STANDARD ENGINEERING PRACTICE
The saturated transponder e.i.r.p. and Received Signal Power is measured
under all weather conditions at the SES Satellite Control Facility in
Betzdorf, Luxembourg. The measured e.i.r.p. for the Customer's
Transponder is kept on record.
In order to accurately determine each transponder e.i.r.p., a measurement
set-up consisting of a calibrated fluxmeter and radiometer is used. The
fluxmeter measures the power flux density at earth surface created by each
individual satellite transponder.
The radiometer measures atmospheric attenuation along the satellite path,
assuming the atmosphere to be an absorbing homogeneous medium at a constant
temperature. Atmospheric attenuation is measured at the beginning of each
e.i.r.p. measurement cycle.
The fluxmeter uses a calibrated antenna, with a calibrated RF measurement
subsystem comprising, among others, a LNA, a down converter and a true RMS
power sensor. A 33 MHz selectivity bandpass filter is used to reduce
errors due to adjacent channel interference during e.i.r.p. measurements.
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SCHEDULE II: CUSTOMER SIGNALS, CUSTOMER UPLINK SIGNALS AND UPLINK FACILITIES
A. SPECIFICATIONS OF CUSTOMER SIGNALS AND CUSTOMER UPLINK SIGNALS
To ensure consistent and uniform reception of high quality video, audio and
data services by the users of ASTRA transmitted services, and to allow full
inter-operability between different manufacturer's equipment, SES requires
each Customer Signal and Customer Uplink Signal to meet the applicable
provisions of the following specifications.
ISO/IEC 13818-1/-2/-3
Generic coding of moving pictures and associated audio (Part 1: Systems:
Part 2: Video and Part 3: Audio).
ETS 300 421
Digital broadcasting systems for television, sound and data services:
framing structure, channel coding and modulation for 11/12 GHz satellite
services.
ETS 300 468
Digital broadcasting systems for television, sound and data services;
specification for Service Information (SI) in Digital Video Broadcasting
(DVB) Systems.
ETR 154
Implementation guidelines for the use of MPEG-2 Systems, video and audio in
satellite and cable broadcasting applications.
ETR 211
Guidelines on implementation and usage of service information.
The Customer agrees to transmit the ASTRA Network Information Table ("NIT")
as described in SCHEDULE IX. More specifically, the Customer Uplink Signals
shall automatically update its transmitted NIT to reflect any changes of
the ASTRA NIT. However, the Customer may modify the parts of the NIT
describing the Customer Uplink Signals (e.g. addition of service list
descriptor).
B. CUSTOMER SIGNALS
1. Video source coding shall be as specified in MPEG-2 main profile/main
level.
2. Audio source coding shall be as specified in ISO/IEC 13818-3 and as
defined in ETR 154.
C. CUSTOMER UPLINK SIGNAL AND UPLINK FACILITIES
The Customer shall comply with the specifications and parameters set-out in
the ASTRA Access Agreement, a copy of which has been separately provided to
the Customer, which may be amended by SES, as necessary, provided that such
amendment also applies to other customers on the Satellite.
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More specifically, the Customer Uplink Signals and the Uplink Facilities
having access to the ASTRA satellite shall meet the performance
requirements established in the ASTRA Access Agreement. SES will provide a
reasonable prior notice for any amendment requiring a change of hardware.
The following parameters shall also be met:
1. EARTH STATION EIRP
For access to the Satellite, the Uplink Facilities must be able to produce
a minimum earth station e.i.r.p. of to be notified by SES to the Customer
once the Customer has informed SES of the uplink site dBW per RF channel
for transmissions originated from to be notified by the Customer to SES
before OSD.
However, given that the Service(s) can be transferred to another ASTRA
satellite, pursuant to CLAUSE 10.5, such transfer may require a separate
earth station and the Customer should note that for such satellite the
Uplink Facilities must be able to produce a minimum earth station e.i.r.p.
to be determined by SES, which may differ from that of the earth station
which accesses the Satellite.
2. TRANSMISSION STANDARD
The transmission standard used for the video, audio, and data services
shall be in accordance with the specifications given in Section A above.
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SCHEDULE III: SERVICE(S) (CLAUSE 10)
The Customer's Transponder shall be used exclusively for the transmission of
the following packages of television services, and related audio, and other
services as specified below all of them targeting at the general public located
within the Target Market. The expression ""Target Market'' means any or all of
the following countries: Poland, Czech Republic, Slovakia, Hungary, Romania,
Moldova, Bulgaria, Belarus, Russia, Ukraine, Estonia, Latvia, Lithuania,
Slovenia, Croatia, Bosnia Herzegovina, Yugoslavia, Macedonia and Albania. It is
understood that those countries are only to such extent part of the Target
Market as they are covered by the Satellite footprint.
A. PAY-PER-VIEW SERVICES, being television services for which the viewer pays
on the basis of the actual consumption.
B. PAY TV SERVICES, being encrypted television services available upon
subscription.
C. UNENCRYPTED SERVICES, being television services available without any
special decoding equipment.
D. OTHER SERVICES: [TBD]
For each service considered, the Customer shall provide SES with the name of
the service, the types of service (pay-per-view, pay TV, unencrypted), the
nature of the programming and the language(s) of the service.
The above information, for any given Service, shall be provided at least 30
days before the proposed start date for the Service and shall be subject to
SES' consent which shall not be unreasonably withheld or delayed and, where
required, to the approval of the Government of Luxembourg. Any change of
service shall be subject to the prior written consent of SES which shall not be
unreasonably withheld or delayed.
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SCHEDULE IV: MONITORING (CLAUSE 8)
In addition to performing the activities related to controlling the Satellite,
SES will also monitor all the transmissions through all its transponders as
described below.
SES will maintain a Network Operations Centre (NOC) capable of monitoring the
Received Signal Power of the Customer's Transponder on a continual basis in
order to produce a computerized record of the RF characteristics of the
Customer's Transponder.
As part of these activities, SES conducts a quarterly test using its In Orbit
Test System (IOTS) of the performance of each transponder on the ASTRA satellite
system. This test will necessitate that the Customer's Uplink Signal be switched
off during selected periods of time in accordance with CLAUSE 8.1 for not more
than thirty (30) minutes at a time.
If a problem is detected, the NOC Operators will initiate and co-ordinate
corrective measures in co-operation with the Uplink Facility which is
transmitting the Customer Uplink Signals.
The NOC's specific functions and responsibilities will include:
- Receiving and handling reports of Unavailability from customers
- Co-ordinating the remedy of the reported difficulty and initiating any
necessary procedures required to restore lost or impaired service in the
most expedient manner
- Maintaining a complete and accurate record of all reported and observed
service failures, impairments, and customer contacts
- Co-ordinating the overall line-up, pre-service tests, and actual provisions
of service
- Arranging the routine monitoring of the Customer's Transponder as described
above
- Ensuring that any potential events that may affect the operation of the
Satellite as a whole or of the Customer's Transponder (sun transit, routine
testing, etc.) are notified to the Customer as soon as practicable and in
advance if possible
The reporting points for operational purposes shall be:
At the Customer: c/o Baker McKenzie
ul. Dluga 26/28
00-238 Warsaw
Tel: (48) 22 635 3521
(48) 22 635 4111
Fax: (48) 22 635 9447
(48) 39 121 1213
At SES: Network Operations Centre
Satellite Control Facility
L-6815 Chateau de Betzdorf
Luxembourg
Tel: for urgent problems only:
(352) 710 152
Tel: for normal operating and general use:
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Tel: (352) 710 725-344
Fax: (352) 710 725-227
(352) 710 725-213
Attn: Head Network Operations Centre
The above telephone and facsimile numbers are subject to change by SES or the
Customer.
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SCHEDULE V: CONDITIONAL ACCESS SYSTEM
The Customer may encrypt the Customer Signals using such system as it shall
reasonably select, in conjunction with SES, SES' approval not to be unreasonably
withheld or delayed. The conditional access system selected shall be DVB
compliant (based upon the DVB common scrambling algorithm and mechanisms). A
conditional access system cannot be applied to the Customer Signals during the
time period where SES provides, in its ground station in Betzdorf, encoding and
multiplexing of the Customer Signals.
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SCHEDULE VI: CHARGES (CLAUSE 4)
A. The charge payable by the Customer to SES in each year of this Agreement
(being a year which commences on CSD or any anniversary of that date) shall
be the sum of the fees to be determined in accordance with paragraphs (i)
and (ii), subject always to paragraph (iii):
[@Entertainment has requested confidential treatment for trade secrets and
commercial or financial information located here.]
(iii) The aggregate charges payable by the Customer to SES in any year
shall not exceed 6,750,000 USD.
B. The Customer shall effect payment of all charges to the bank account
identified by SES in the corresponding invoice.
C. The daily rate of charge to be applied for the purposes of calculating any
refund to be made pursuant to Clause 6 of the Agreement shall be the
aggregate charges payable for the Payment Period in the course of which an
Unavailability occurred divided by the number of
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days contained in said Payment Period.
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SCHEDULE VII: PRIORITY AND PRE-EMPTION
A. CUSTOMER STATUS
The Customer shall have the status of: Non-pre-emptible Customer as defined in
PART B below.
B. CATEGORIES OF USE
SES' customers using the ASTRA satellite system shall be accorded (for each
transponder used) priority status as: Protected, Non-Pre-emptible or
Pre-emptible.
1. Protected Customers:
a. will not be subject to pre-emption by other customers;
b. will be entitled to be provided with the use of a back-up transponder
(this will require the pre-emption of Pre-emptible Customer); and
c. shall have the benefit of Spare TWTAs, in preference to certain other
customers, as set out in PART C below.
2. Non-Pre-emptible Customers:
a. will not be subject to pre-emption themselves;
b. will have no rights of pre-emption themselves; and
c. shall have the benefit of Spare TWTAs as set out in PART C below.
3. Pre-emptible Customers:
a. have no rights or pre-emption themselves;
b. may have their transponder pre-empted, as set out in PART D below, in
order to provide a back-up transponder to a Protected Customers; and
c. shall have the benefit of Spare TWTAs, but subject to the rights of
other customers in this Schedule, as set out in PART C below.
C. PRIORITY RULES FOR SPARE TWTAs
As a general rule, Spare TWTAs on the Satellite will be provided on a First
failed/first served basis.
However, in the event of simultaneous transponder failures (or where the
sequence of failures cannot be determined) on the Satellite, and if the number
of failures exceeds the number of available Spare TWTAs, then the following
rules shall apply:
1. Protected Customers have priority over Non-Pre-emptible Customers who, in
turn, have priority over Pre-emptible Customers.
2. Where, pursuant to this Schedule, conflicting rights to Spare TWTAs arise
between customers with the same priority status, priority shall be given in
accordance with the following rules:
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a. customers whose service starts on the Operational Service Date
("OSD CUSTOMER") shall have priority over those service starts at a
date after such Operational Service Date;
b. between OSD Customers, priority shall be determined by reference to
the expiry dates of their contracts so that the customers with the
later dates of expiry have priority over customers with earlier expiry
dates;
c. between OSD Customers whose contracts expire on the same date,
priority shall be determined by reference to the dates on which they
signed contracts for the use of a transponder, so that the customers
who signed earlier have priority over those who signed later;
d. between customers whose services start after the Operational Service
Date ("POST OSD CUSTOMERS"), priority shall be determined by reference
to the customer start dates, so that the customers with earlier
customer start dates shall have priority over customers with later
customer start dates;
e. between Post OSD Customers who have the same customer start dates,
priority shall be determined in the same manner as applicable for OSD
Customers under PARAGRAPH 2(b) and (c) above; and
f. between customers originating from different satellites (i.e.
customers whose initial transponder was located on an ASTRA satellite
other than the Satellite), priority shall be determined by reference
to their respective start date on their respective initial satellite,
so that the customers with earlier customer start dates shall have
priority over customers with later customer start dates.
3. For the purpose of the above rules, (i) the expiry date of a contract
shall, in case of extension of the contract, refer to the extended expiry
date, and (ii) the customer start date refers to the start date of a
customer's initial service and is not affected by any subsequent change of
the service transmitted under a given customer contract.
D. PRE-EMPTION RULES
1. If PART A above provides that the Customer has the status of
Pre-emptible Customer, then the Customer's Transponder shall be
pre-emptible on the terms set out below.
2. a. SES shall have the right to pre-empt the Customer's Transponder
to provide back-up capacity to restore the service of a Protected
Transponder in respect of which SES is contractually bound to provide
back-up capacity at the time pre-emption occurs and if there is no
Spare TWTA that can be used to restore the Protected Transponder's
service.
b. As used herein, "PROTECTED TRANSPONDER" means the transponder of a
Protected Customer on another ASTRA satellite, to be nominated by SES
and notified by SES to the Customer at any time, the protection of
which directly or indirectly requires the pre-emption of the
Customer's Transponder. There may be several Protected Transponders
nominated by SES, provided that each is on a different ASTRA
satellite. SES may increase or reduce the number of Protected
Transponders at any time by giving prior written notice to the
Customer.
3. To Pre-empt the Customer's Transponder:
a. SES will give the Customer at least 24 hours advance warning (by
fax or phone) of
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such pre-emption save in the event of consecutive failures of a
Protected Transponder, in which case such pre-emption warning may be
shorter, it being understood that SES will keep the Customer informed
of the status of the Protected Transponders affected by such
consecutive failures; and
b. at the expiry of the aforementioned advance warning, SES shall have
the right to forthwith interrupt the transmission of all video and
audio services using the Customer's Transponder and the Customer shall
therefore forthwith, upon SES' request, interrupt the transmission of
the Customer Uplink Signal. SES shall in addition have the right to
interrupt the reception of the Customer Uplink Signals by the
Customer's Transponder.
4. The Customer shall comply diligently with SES' instructions for the
purposes of implementing the pre-emption and shall require the operator of
the Uplink Facilities to do the same.
5. a. If SES pre-empts the Customers' Transponder, then, at that time, SES'
obligation to provide the use of the Customer's Transponder, and the
Customer's obligation to pay the corresponding charge, shall be
suspended. The Agreement shall terminate 30 days after the pre-emption
date unless SES, within this period, restores the Protected
Transponder in respect of which pre-emption was implemented. If such
restoration occurs after this 30 days period, then SES shall offer the
Customer's Transponder back to the Customer on the terms set out in
this Agreement for the outstanding period of Term. The Customer shall
have fifteen (15) days to accept SES' offer.
b. Upon termination of the Agreement pursuant hereto, as the case may be,
i. SES shall refund to the Customer the pro rate temporis portion of
the advance payments made by the Customer pursuant to SCHEDULE VI
and relating to the unexpired portion of the period (in respect
of which the Customer has paid in advance) in progress on the
date of pre-emption; or
ii. the Customer shall pay to SES all outstanding sums owed to SES at
the time of termination.
6. a. The Customer shall fully cooperate with SES for the exercise, by SES,
of its right of pre-emption provided herein and shall not raise any
objection, initiate any legal proceedings against SES or the Protected
Customer benefiting from the pre-emption, or take other steps, to
prevent, delay or obstruct the exercise of this right and the Customer
shall be liable for all damages suffered by SES or such Protected
Customer in connection therewith.
b. The Customer shall not make any claim against SES or the Protected
Customer benefiting from the pre-emption in connection with the
exercise, by SES, of its right of pre-emption and shall indemnify SES
against any related third party claim.
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SCHEDULE VIII: ASTRA ACCESS AGREEMENT
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SCHEDULE IX: ASIUS
30
[ASTRA LOGO]
ASTRA ACCESS AGREEMENT
PERFORMANCE CHARACTERISTICS OF
EARTH STATIONS HAVING ACCESS TO
ASTRA SATELLITES
--------------------------------------------------------------------------------
ASTRA ACCESS AGREEMENT SOCIETE EUROPEENNE DES SATELLITES
1 AUGUST 1996 CONFIDENTIAL PROPRIETARY
[ASTRA LOGO]
SOCIETE EUROPEENNE DES SATELLITES S.A.
L-6815 CHATEAU DU BETZDORF, LUXEMBOURG
TEL: (352) 710725-1
FAX: (352) 710725-548
ASTRA is a trademark of Societe Europeenne des Satellites.
The information and data contained herein are subject to change.
CONTENTS
[Download Table]
1. INTRODUCTION.......................................................... 1
2. ANTENNA SYSTEM........................................................ 2
2.1. General......................................................... 2
2.2. Frequency Range................................................. 2
2.3. Off-axis Antenna Gain Pattern................................... 4
2.4. Polarisation.................................................... 4
2.5. Motorisation, Antenna Pointing and Tracking..................... 4
3. RF EQUIPMENT.......................................................... 5
3.1. Frequency Range and Agility..................................... 5
3.2. E.i.r.p. Capability............................................. 5
3.3. Transmitter Inhibit............................................. 5
3.4. Out-of-Band e.i.r.p. Emission................................... 6
3.5. Off-axis e.i.r.p. Density....................................... 6
3.6. Frequency Stability............................................. 6
4. AMPLITUDE AND GROUP DELAY DISTORTIONS................................. 7
4.1. FM TV transmission in FSS and BSS bands......................... 7
4.2. Digital transmission in FSS and BSS bands....................... 8
4.3. Group Delay Equalisation........................................ 9
5. BASEBAND PARAMETERS FOR FM TV TRANSMISSION............................ 10
5.1. General......................................................... 10
5.2. PAL Transmission Standard....................................... 10
5.2.1. Video Signal............................................ 10
5.2.1.1. Frequency Deviation........................... 10
5.2.1.2. Energy Dispersal.............................. 10
5.2.1.3. Pre-emphasis.................................. 11
5.2.2. On-line Testing......................................... 11
5.2.3 Audio Signals........................................... 11
5.2.3.1. Audio Channel Modes........................... 11
5.2.3.2. Subcarrier Frequency.......................... 15
5.2.3.3. Subcarrier Bandwidth.......................... 16
5.2.3.4. Subcarrier Modulation Index................... 16
5.2.3.5. Analogue Audio................................ 16
5.2.3.5.1. Analogue Audio Deviation.......... 16
5.2.3.5.2. Analogue Audio Bandwidth.......... 16
5.2.3.5.3. Pre-emphasis...................... 16
5.2.3.6. Digital Audio................................. 17
5.2.3.6.1. Sampling Method................... 17
5.2.3.6.2. Modulation Method................. 17
5.2.3.6.3. Auxiliary Data.................... 17
5.2.3.7. Network Control Carrier....................... 17
5.2.4 Teletext................................................ 17
--------------------------------------------------------------------------------
ASTRA ACCESS AGREEMENT SOCIETE EUROPEENNE DES SATELLITES
1 AUGUST 1996 CONFIDENTIAL PROPRIETARY
i
[Download Table]
6. CHANNEL CODING, MODULATION, MULTIPLEXING AND SOURCE CODING
FOR DIGITAL SERVICES.................................................. 18
6.1. General......................................................... 18
6.2. Modulation...................................................... 18
6.2.1. BSS bands............................................... 18
6.2.2. FSS bands............................................... 18
6.2.3. Earth Station Degradation............................... 18
6.3. Channel coding.................................................. 18
6.4. Power Spectrum Density Mask..................................... 19
6.4.1. BSS Bands............................................... 19
6.4.2. FSS Bands............................................... 19
6.5. Multiplexing.................................................... 20
6.5.1. General................................................. 20
6.5.2. Transport Stream........................................ 20
6.5.3. Service Information..................................... 20
6.6. Source Coding................................................... 21
7. ASTRA SATELLITE INFORMATION........................................... 22
7.1. ASTRA 1 series.................................................. 22
7.1.1. ASTRA 1 Transponder Frequency Plan...................... 22
7.2. ASTRA 2 series.................................................. 31
7.2.1. ASTRA 2 Transponder Frequency Plan...................... 31
8. ORBITAL POSITION / STATION KEEPING.................................... 35
9. BEACON INFORMATION.................................................... 35
9.1. ASTRA 1A and ASTRA 1B Beacon Details............................ 36
9.2. ASTRA 1C, 1D, 1E, 1F, 1G and 1H Beacon Details.................. 36
9.3. ASTRA 2A Beacon Details......................................... 36
9.4. ASTRA 2B Beacon Details......................................... 37
Annex 1.................................................................... 38
MULTIPLEX DIAGNOSTIC TABLE (MDT)...................................... 38
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1. INTRODUCTION
In order to access an ASTRA satellite, approval must first be obtained from
Societe Europeenne des Satellites - SES. The purpose of this approval is to
control the technical parameters of the Uplink Facilities and Customer's Uplink
Signal, to ensure that the following objectives are met:
- The desired signal quality and availability are achieved;
- Harmful interference is not produced in the other transmissions carried by
any ASTRA spacecraft;
- The interference produced in other satellite systems will not exceed the
coordinated levels.
This document outlines the specifications established by SES in order to achieve
those objectives. Access to a specific ASTRA satellite will only be granted
after compliance to the specifications has been demonstrated to the satisfaction
of SES.
In case of contradiction between the ASTRA Access Agreement and the Customer's
Transponder Agreement, the latter shall prevail.
The following definitions are utilised in this document:
OPERATOR - Person, firm, corporation or other legal entity using an ASTRA
transponder.
SATELLITE CONTROL FACILITY (SCF) - SES earth station complex located at
Betzdorf, Grand Duchy of Luxembourg.
DIGITAL TRANSMISSION FACILITY (DTF) - Part of the SES earth station complex,
located at Betzdorf, Grand Duchy of Luxembourg, in which digital services are
handled.
ANALOGUE NETWORK OPERATIONS CENTRE (NOC) - The monitor and control center for
all analogue ASTRA services, located at the SCF. This provides a 24 hour monitor
and control network reporting point for service quality monitoring and problem
resolution for the ASTRA analogue satellites.
DIGITAL NETWORK OPERATIONS CENTRE (DINO) - The monitor and control centre for
all ASTRA digital services, located at the DTF. This provides a 24 hour monitor
and control network reporting point for service quality monitoring and problem
resolution for the ASTRA digital satellites.
REFERENCE STANDARD EARTH STATION (RSES) - These stations are highly maintained
up- and downlinks to be used in developing baseline performance standards for
transmissions carried by the ASTRA satellites.
ASTRA ACCESS AGREEMENT SOCIETE EUROPEENNE DES SATELLITES
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[Download Table]
SATELLITE REFERENCE STANDARD EARTH STATION
--------- --------------------------------
ASTRA 1A...........................BTZ # 2
ASTRA 1B...........................BTZ # 3
ASTRA 1C...........................BTZ # 4
ASTRA 1D...........................BTZ # 5
ASTRA 1E...........................BTZ # 6
ASTRA 1F...........................BTZ # 10
ASTRA 1G...........................BTZ # 12
ASTRA 1H...........................BTZ # 14
ASTRA 2A...........................BTZ # 13
ASTRA 2B...........................BTZ # 15
Table 1. ASTRA REFERENCE STANDARD EARTH STATIONS
2. ANTENNA SYSTEM
2.1 GENERAL
A dedicated antenna system shall be used for access to any ASTRA satellite.
Simultaneous access to two or more ASTRA satellites by a single antenna system
is not permitted, but it is permitted for one antenna to access a single
spacecraft in both the FSS and BSS bands. By using a dedicated antenna system as
specified herein for a given ASTRA satellite, link performance in terms of
uplink and downlink Carrier/Thermal Noise (C/N) and Carrier/Cross Polar
Interference (C/X) can be maintained.
2.2 FREQUENCY RANGE
The antenna system is required to meet all the specifications set in the next
items operating in the appropriate FSS or BSS frequency range.
The uplink frequency ranges for the different ASTRA satellites (primary and
back-up bands) are shown in the following Table 2.
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[Download Table]
FSS BSS
Satellite 12.75-13.25 13.75-14.00 14.00-14.50 17.30-18.10
ASTRA 1A..... A-Band
ASTRA 1B..... B-Band
ASTRA 1C..... C-Band A-Band
ASTRA 1D..... D-Band C-Band B-Band E-Band
ASTRA 1E..... D-Band C-Band B-Band E-Band
ASTRA 1F..... A-Band E-Band F-Band
ASTRA 1G..... G-Band E-Band F-Band
ASTRA 1H..... G-Band E-Band F-Band
ASTRA 2A..... G-Band E-Band F-Band
ASTRA 2B..... G-Band B-Band E-Band F-Band
Table 2. ASTRA Uplink Frequency Bands
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2.3. OFF-AXIS ANTENNA GAIN PATTERN
The gain, (expressed in dBi), relative to an isotropic antenna, at any off-axis
angle (-) (expressed in degrees) shall comply with the following:
[Download Table]
FREQUENCY RANGE (GHz) GAIN (dBi) ANGULAR RANGE
--------------------- ---------- -------------
14.00 - 14.50 . . . . . G </- 29 - 25 log (-) 1 degree < (-) </- 20 degrees
G </- 32 - 25 log (-) 20 degrees < (-) </- 48 degrees
G </- -10 48 degrees < (-) </- 180 degrees
12.75 - 13.25 . . . . . G </- 29 - 25 log (-) 0.5 degrees < (-) </- 36.3 degrees
13.75 - 14.00 . . . . . G </- -10 36.3 degrees < (-) </- 180 degrees
17.30 - 18.10 . . . . . G </- 29 - 25 log (-) 1 degree < (-) </- 36.3 degrees
G </- -10 36.3 degrees < (-) </- 180 degrees
2.4. POLARISATION
The ASTRA satellites employ dual linear orthogonal polarisation. The antenna
polarisation angle will be set with SES during service line-up, following the
appropriate procedure established by the NOC and the DINO. The cross-polarised
signal component transmitted by the antenna shall be as specified below:
FSS band: 30 dB
BSS band: 35 dB
2.5. MOTORISATION, ANTENNA POINTING AND TRACKING
Permanent uplink antennas shall be motorised in both azimuth and elevation to
enable rapid repointing in case of necessity, and to facilitate accurate antenna
pattern measurements.
Further, the utilisation of a suitable tracking system is recommended in order
to meet the e.i.r.p. stability requirement specified in the following section
3.2. The tracking system design shall be based on the ASTRA satellite station
keeping and beacon frequency parameters, which are presented in sections 8 and 9
respectively. It shall guarantee the clear sky polarisation value specified in
the previous section 2.4.
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3. RF EQUIPMENT
The RF equipment, including any redundant equipment, is required to meet all
the specifications set out in the following sections 3.1 to 3.6.
3.1. FREQUENCY RANGE AND AGILITY
It shall be possible to set the carrier centre frequency to within +-125 kHz.
3.2. E.I.R.P. CAPABILITY
The e.i.r.p. will be established by SES based on the utilised channel and on
the uplink geographical location.
It is expected that SES may request changes in the earth station e.i.r.p.
during the course of the contract, to account for changes in the transponder
performance over its lifetime, utilisation of redundant units or utilisation of
a different transponder.
The uplink e.i.r.p. stability shall be equal to or better than +-0.5 dB
including antenna pointing and tracking errors.
Means shall be provided to allow adjustment of the carrier level to within 0.5
dB of the specified value.
3.3. TRANSMITTER INHIBIT
Operators accessing ASTRA satellites may be required by the NOC or the DINO to
shut down a transmission in the case where it is producing harmful interference
into other transmissions. Shut down of a transmission may also be required to
allow the switching into operation of redundant units in the satellite.
In order to comply with this requirement, the Operator shall provide
continuous manning of the uplink site or a remote control system to another
location which will be manned continuously.
The transmitter shall utilise a system which automatically inhibits the
transmission of a chain upon the detection of failure conditions such as loss
of phase lock on an upconverter or excessive HPA transmit power. This system may
also be designed to, alternatively, switch the transmission to a stand-by chain.
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3.4. OUT-OF-BAND E.I.R.P. EMISSION
Earth station out-of-band emissions are additional sources of interference for
other carriers utilising ASTRA transponders. The two contributions to
out-of-band e.i.r.p. emission are spurious output and intermodulation products.
Note that the specification applies across all ASTRA uplink bands (both FSS and
BSS) for all stations. The specified limits for these two contributions are the
following:
-- The out-of-band on-axis e.i.r.p. emissions in the 12.75 - 13.25, 13.75 -
14.50, and 17.30 - 18.10 GHz bands, resulting from spurious output, must
not exceed 4.0 dBW/4 kHz;
-- The out-of-band on-axis e.i.r.p. emissions in the 12.75 - 13.25, 13.75 -
14.50, and 17.30 - 18.10 GHz bands, resulting from intermodulation
products, must not exceed 12.0 dBW/4 kHz.
3.5. OFF-AXIS E.I.R.P. DENSITY
This parameter has a direct impact on the interference produced in other
satellite systems. In order to keep this interference within acceptable levels,
the earth station must comply with the following e.i.r.p. limits. The off-axis
angle, (-), is referred to the main lobe axis, in degrees.
For the frequency range 14.00 - 14.50 GHz, based on ITU-R Report 1001:
[Download Table]
35 - 25log (-) dBW/40 kHz for 2.5 degrees </- (-) </- 48 degrees
-7 dBW/40 kHz for 48 degrees < (-) </- 180 degrees
For the frequency range 12.75 - 13.25 GHz based on the ITU Appendix 30B planned
limits (averaged over the necessary bandwidth of 26 MHz:
[Download Table]
-25 - 25log (-) dBW/kHz for 0.5 degrees </- (-) </- 36.3 degrees
-64 dBW/kHz for 36.3 < (-) </- 180 degrees
For the frequency range 13.75 - 14.00 GHz, the antenna must fully comply with
the antenna specification (section 2.3).
For the frequency range 17.30 - 18.10 GHz, the input power to the antenna shall
not exceed 30 dBW in a single transponder, and the antenna must conform fully
with the antenna specification (section 2.3).
3.6. FREQUENCY STABILITY
The RF frequency tolerance of the transmitted carrier shall be equal to or
better than +/- 150 kHz, long and short term stability.
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4. AMPLITUDE AND GROUP DELAY DISTORTIONS
4.1. FM TV TRANSMISSION IN FSS AND BSS BANDS
The earth station IF uplink filter shall be provided in the uplink chain and
shall conform to the amplitude limits shown in Figure 4.1.1.
The group delay produced by transmit earth station IF and RF equipment --
including the up-converter, IF filter, HPA, RF filter combiners, feed and
transmission lines -- shall be equalised to the limits given in Figure 4.1.2.
[FIGURE 239A]
[Download Table]
FREQUENCY (MHz) AMPLITUDE (dB)
---------------------------- ----------------------------
A B C D a b c d
---- ---- ---- ---- --- --- --- ----
20.2 25.2 28.9 40.0 0.2 2.2 8.3 25.0
Figure 4.1.1 IF UPLINK FILTER AMPLITUDE RESPONSE
[FIGURE 239B]
[Download Table]
FREQUENCY (MHz) GROUP DELAY (ns)
---------------------------- ----------------------------
A/3 A H f g h
----- ---- ----- --- --- ----
6.7 20.2 24.6 2.0 3.0 12.0
Figure 4.1.2 IF UPLINK FILTER GROUP DELAY RESPONSE
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4.2. DIGITAL TRANSMISSION IN FSS AND BSS BANDS
For the FSS or BSS transmit channel from upconverter input to antenna output,
the total amplitude and group delay distortions shall not exceed the values
specified in Table 4.2.1.
[Download Table]
FSS BSS
------------ -----------
FREQUENCY (MHZ)................. 26 30 33 39
Amplitude variation (dB pp)...... 0.5 0.7 0.5 0.7
Group delay variation (nss pp)... 6.0 8.0 6.0 8.0
Table 4.2.1 AMPLITUDE AND GROUP DELAY DISTORTIONS
In the case where an RF channel filter network is used, the amplitude and group
dealy masks specified in Figure 4.2.1 and 4.2.2 shall be met from the HPA output
to the antenna output.
(FIGUE 240)
[Download Table]
BAND FREQUENCY (MHz) AMPLITUDE (dB)
------------------------ -----------------------
A B C a b c
--- --- --- --- --- ---
FSS........... 26 30 114 0.25 0.35 35
BSS........... 33 39 123
Figure 4.2.1 RF CHANNEL FILTER AMPLITUDE RESPONSE
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[FIGURE 241]
[Download Table]
BAND FREQUENCY (MHz) GROUP DELAY (ns)
---- ----------------- ------------------
A B a b
--- --- --- ---
FSS............. 26 30 3.5 5.0
BSS............. 33 39
Figure 4.2.2. RF CHANNEL GROUP DELAY MASK
4.3 GROUP DELAY EQUALISATION
Equalisation capability shall be provided at the earth station for intrinsic
group delay in the earth station transmit equipment and for group delay in the
satellite transponder.
The maximum range of satellite group delay to be equalised at the earth station
is given below:
-- Linear : +/-1.0 ns/MHz
-- Parabolic : 0.5 ns/MHz(2)
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5. BASEBAND PARAMETERS FOR FM TV TRANSMISSION
5.1. GENERAL
In general the baseband television signal parameters defined shall be designed
in accordance with the relevant definitions and standards for that system and
as authorised by SES.
5.2. PAL TRANSMISSION STANDARD
5.2.1 VIDEO SIGNAL
The transmitted video signal shall correspond to that of ITU-R Report 624-4 and
Recommendation 472-3, using PAL values with a maximum video signal bandwidth of
5 MHz.
A lowpass filter at the video input to the modulator shall reject any signal
above 6 MHz by at least 40 dB. Up to 5 MHz this filter shall have a group
ripple of less than +/-20 ns.
The following items present information concerning the basic modulation
parameters.
5.2.1.1. FREQUENCY DEVIATION
The utilised peak-to-peak frequency deviation for the video signal shall be 16
MHz/V, assuming the difference between white and black levels to be 0.7 V.
5.2.1.2. ENERGY DISPERSAL
The earth station shall be equipped to add to the TV signal a fixed amplitude
symmetrical triangular waveform, phase locked to the video frame rate, capable
of producing the specified peak-to-peak deviation of the television carrier.
The utilised frequency of that waveform shall be 25 Hz.
-- In the presence of a modulating signal: 2.0 MHz
-- In the absence of a modulating signal: 4.0 MHz
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5.2.1.3. PRE-EMPHASIS
The utilised pre-emphasis network shall be that defined in the ITU-R
Recommendation 405-1 (625 lines).
5.2.2. ON LINE TESTING
In order to enable service performance monitoring while on-line transmission is
present, vertical interval test signals (VITS) shall be inserted on the
transmitted baseband video signal. These signals are based on ITU-R
Recommendation 473-5, as depicted in Figures 5.2.2.1 - 5.2.2.3 and shall utilise
one of the following VITS line modes:
[Download Table]
Test signal Line Line Line
----------- ---- ---- ----
CCIR 17............17 18 19
CCIR 18............18 or 19 or 20
CCIR 330...........330 331 332
CCIR 331...........331 332 333
In addition line 22 shall always be used as a "quiet" line to allow the
measurement of end-to-end signal/noise ratio or for other purposes specified by
SES.
5.2.3. AUDIO SIGNALS
5.2.3.1. AUDIO CHANNEL MODES
The TV carrier shall (normally) be supplemented by a number of audio channels.
The following sections describe the various subcarrier configurations that may
be used for the transmission of audio channels for both TV-related and non
TV-related applications.
Only those subcarriers specified in the Customer's Transponder Agreement shall
be utilised and only subcarrier modulation equipment approved by SES shall be
employed.
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[Enlarge/Download Table]
Characteristics measured Waveform used Line number
------------------------ --------------------------------------- ---------------
Linear distortions
Insertion gain............................ B(2) Bar 17 and 330
Amplitude/frequency response.............. C(2) and C(1) Multiburst 18
Line-time waveform distortion............. B(2) Bar 17 and 330
Short-time waveform distortion:
-- step response........................ B(2) Bar 17 and 330
-- pulse response....................... B(1) 2T 17 and 330
Chrominance-luminance gain inequality..... B(2) and G, or G(2) Bar & Subcarr. 17 and 330, 331
B(2) and F Bar & 20T 17
Chrominance-luminance delay inequality.... F 20T 17
Non-linear distortions
Luminance line-time non-linearity......... D(1) Staircase 17
Chrominance non-linearity................. G(2) 3 Step Subcarr. 331
Luminance-chrominance intermodulation:
-- differential gain.................... D(2) Modulated 330
-- differential phase................... D(2) and E Staircase 330, 331
Chrominance-luminance intermodulation..... B(2) and G(1) or G(2) Bar & Subcarr. 17,331
Table from CCITT-Rec No. 67
Figure 5.2.2.1 VERTICAL INTERVAL TEST SIGNALS
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[FIGURE 249A]
[FIGURE 245B]
Figure 5.2.2.2. VERTICAL INTERVAL TEST SIGNALS
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[FIGURE 246A]
[FIGURE 246B]
Figure 5.2.2.3. VERTICAL INTERVAL TEST SIGNALS
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5.2.3.2. SUBCARRIER FREQUENCY
The audio subcarriers shall utilise only the frequencies presented in Table
5.2.3.2.1, and shall only be used in the manner indicated in column "Type'',
and in accordance with Section 5.2.3.1.
[Download Table]
TYPE FREQUENCY (MHZ)
Digital Only......................................................... 6.12@
Digital Only......................................................... 6.30@
Digital Only......................................................... 6.48@
Digital Only......................................................... 6.66@
Digital Only......................................................... 6.84@
TV sound (A:L/M)..................................................... 7.02
TV sound (A:R/M)..................................................... 7.20
D or A (L/M)......................................................... 7.38
D or A (R/M)......................................................... 7.56
D or A (L/M)......................................................... 7.74
D or A (R/M)......................................................... 7.92
Digital Only......................................................... 8.10*
Digital Only......................................................... 8.28*
Digital Only......................................................... 8.46#
Low Speed Data for network control.................................... 8.595#
Table 5.2.3.2.1 SUBCARRIERS FREQUENCIES
A = analogue companded system with Panda(R)-1 parameters.
D = digital stereo 192 kbit/s QPSK signal using ISO 11172-3 Layer II
parameters.
L = left stereo R = right stereo M = mono
* - Frequency tolerance of +/-0.005 MHz for all subcarriers
@ - As an option these five subcarriers may be replaced by a single
non-companded analogue subcarrier at 6.50 MHz used for mono TV sound.
# - In some applications the use of this subcarrier may be restricted to
prevent degradation of the picture quality.
(R) - Panda is a registered trademark of WEGENER Communications Inc.
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5.2.3.3. SUBCARRIER BANDWIDTH
A 130 kHz nominal bandwidth shall be utilised for all the analogue companded or
digital audio subcarriers. In the case of the non-companded mono subcarrier, the
nominal bandwidth of the modulated signal shall be 200 kHz.
5.2.3.4. SUBCARRIER MODULATION INDEX
The modulation index of the subcarrier, BETAsc, is given by the following
expression:
BETAsc = Osc/Fsc
Where Osc is the peak deviation produced by the subcarrier in the TV carrier and
Fsc is the frequency of the subcarrier, both Osc and Fsc being given in MHz.
For the analogue companded subcarriers, a modulation index of 0.15 shall be
utilised. For the digital audio subcarriers, a modulation index of 0.12 shall be
utilised. For the network control subcarrier (8.595 MHz) a modulation index 0.10
shall be utilised. In the case of the non-companded mono subcarrier a modulation
index of 0.26 shall be utilised.
5.2.3.5. ANALOGUE AUDIO
5.2.3.5.1 ANALOGUE AUDIO DEVIATION
The peak frequency deviation produced by a 9 dBm0 test on the analogue companded
subcarriers shall be +/- 50 kHz. In the case of the non-companded mono
subcarrier, a 9 dBm0 test tone shall produce a peak frequency deviation of
+/- 85 kHz.
5.2.3.5.1 ANALOGUE AUDIO BANDWIDTH
All the analogue audio channels shall provide an audio baseband ranging from
20 Hz to 15 kHz.
5.2.3.5.3. PRE-EMPHASIS
The analogue companded subcarriers shall utilise 75 mu's together
with an adaptive pre-emphasis compatible with the WEGENER Communications
Panda(R)-l system. The pre-emphasis time constant of the non-companded audio
subcarrier shall be 50 mu's.
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5.2.3.6. DIGITAL AUDIO
The digital audio subcarriers shall utilise ISO 11172-3 Layer II coding system
to achieve a CD quality stereo channel and shall conform with the SES document
"ASTRA DIGITAL RADIO (ADR)".
5.2.3.6.1. SAMPLING METHOD
The analogue stereo signal input shall be sampled at a rate of 48 ksamples/s.
Compression based on the ISO 11172-3 Layer II algorithm shall then be performed
to generate a 192 kbit/s digital stereo signal.
5.2.3.6.2 MODULATION METHOD
The digital audio signals shall be modulated using the differential QPSK method,
with a convolutional code of rate 3/4, with constraint length 7. CCITT V.35
scrambling shall be employed. An appropriate filter mask shall be applied in the
modulator to limit the bandwidth to the same value as for an analogue companded
subcarrier.
5.2.3.6.3. AUXILIARY DATA
The format of any auxiliary data in the ISO 11172-3 Layer II data stream shall
be agreed by SES in writing.
5.2.3.7. NETWORK CONTROL CARRIER
The maximum data rate shall be 14.4 kbit/s using asynchronous FSK modulation.
The modulation index shall be 0.10.
5.2.4 TELETEXT
The Teletext signal shall conform to the specifications for Teletext System B as
defined in ITU-R Recommendation 653, for the case of a 625/50 television system.
THE VBI (VERTICAL BLANKING INTERVAL) SHALL NOT BE USED FOR TRANSMISSION OF ANY
OTHER TYPE OF INFORMATION OR SIGNAL WITHOUT PREVIOUS AUTHORISATION IN WRITING
FROM SES.
Teletext signals shall only be inserted between lines 7 and 21 inclusive (and
the corresponding lines in the second field) other than on those lines used for
VITS test signals as specified in paragraph 5.2.2 unless specifically approved
in writing by SES.
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6. CHANNEL CODING, MODULATION, MULTIPLEXING AND SOURCE CODING FOR DIGITAL
SERVICES
6.1. GENERAL
Channel coding and modulation equipment shall conform to the following
specifications:
ETS 300 421
Digital broadcasting systems for television, sound and data services;
Framing structure, channel coding and modulation for 11/12 GHz satellite
services.
ETR 154
Digital broadcasting systems for television; Implementation guidelines for
the use of MPEG-2 systems; Video and audio in satellite and cable
broadcasting applications.
The transmitted RF carrier spectrum shall not be inverted with respect to the
modulator output spectrum. The phase accuracy at the modulator output shall be
+/- 2 degrees. The amplitude accuracy at the modulator output shall be +/- 0.2
dB.
6.2. MODULATION
6.2.1. BBS BANDS
The modulation shall be QPSK at a transmission bit rate of 55.0 Mbit/s, in order
to operate with a single carrier at a fixed symbol rate of 27.5 Msym/s.
6.2.2. FSS BANDS
The modulation shall be QPSK at a transmission bit rate of 44.0 Mbit/s, in order
to operate with a single carrier at a fixed symbol rate of 22.0 Msym/s.
6.2.3. EARTH STATION DEGRADATION
The Eb/No degradation (for the case of FEC 3/4 and BER = 10(7)) caused by the
earth station equipment shall be less than 0.5 dB. This value shall be verified
in a station loop including baseband, IF and RF equipment of the uplink and
downlink chain.
6.3. CHANNEL CODING
Forward Error Correction (FEC) shall conform to the specifications given in
section 6.1 and shall permit the use of one or more of the following FEC ratios;
1/2, 2/3, 3/4 or (in the case of FSS 26 MHz bandwidth) 5/6.
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6.4 POWER SPECTRUM DENSITY MASK
6.4.1 BSS BANDS
To avoid adjacent channel interference, the RF spectrum at the output of the
power amplifier of the earth station shall not exceed the tolerance mask shown
in Fig. 6.4.1. It may be necessary to operate the power amplifier in back-off
mode in order to achieve this specification.
[Download Table]
Frequency Offset (+/-) Amplitude
(MHz) (dB)
---------------------- --------- [FIGURE 251A]
0 - 19.50 0.0
19.50 - 29.25 -25.0
>/- 40.00 -40.0 FIGURE 6.4.1 BSS POWER SPECTRUM MASK
6.4.2 FSS BANDS
To avoid adjacent channel interference, the RF spectrum at the output of the
power amplifier of the earth station shall not exceed the tolerance mask shown
in Fig. 6.4.2. It may be necessary to operate the power amplifier in back-off
mode in order to achieve this specification.
[Download Table]
Frequency Offset (+/-) Amplitude
(MHz) (dB)
---------------------- --------- [FIGURE 251B]
0 - 14.75 0.0
14.75 - 22.50 -25.0
>/- 30.00 -40.0 FIGURE 6.4.2 FSS POWER SPECTRUM MASK
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6.5. MULTIPLEXING
6.5.1. GENERAL
Multiplexing of video, audio, and data signals shall conform to the following
specifications:
ISO/IEC 13818-1
Generic coding of moving pictures and associated audio (Part 1: Systems).
ETR 154
Digital broadcasting systems for television; Implementation guidelines for
the use of MPEG-2 systems; Video and audio in satellite and cable
broadcasting applications.
6.5.2. TRANSPORT STREAM
The Transport Stream (excluding error correcting code overhead) shall operate at
one of the following bit rates, dependent on the FEC to be used:
[Download Table]
Transport Stream bit rate
FEC ratio (Mbit/s)
--------- -------------------------
BSS FSS
----- -----
1/2............ 25.34 20.27
2/3............ 33.79 27.03
3/4............ 38.01 30.41
5/6............ n.a. 33.79
6.5.3. SERVICE INFORMATION
Service Information shall conform to the following specifications:
ETS 300 468
Digital broadcasting systems for television, sound and data services;
Specification for Service Information (SI) in Digital Video Broadcasting
(DVB) systems.
ETR 211
Digital broadcasting systems for television; Implementation guidelines for
the use of MPEG-2 systems; Guidelines on implementation and usage of
service information.
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It is further required to receive the original ASTRA NETWORK INFORMATION TABLE
(NIT) uplinked from Betzdorf and to re-transmit this table in intervals of at
least 10 seconds on each locally uplinked ASTRA transponder.
The last version of the original NIT should be kept in memory. This ensures an
uninterrupted availability of the NIT in case the original NIT cannot be
received.
By means of the local service Information editing station, the transponder
specific parts of the NIT can be modified/updated at any time.
A MULTIPLEX DIAGNOSTIC TABLE (MDT) has been defined to provide a mechanism for
conveying diagnostic information about the consistency of all multiplexes to the
central Network Operations Centre at Betzdorf.
The local uplinks should generate such MDT in the case a service failure occurs
for longer than 10 seconds, i.e. if a service component (video, audio, subtitle
or accompanied data) or a Service Information component (NIT, SDT, EIT or TDT)
is missing.
This involves that the local encoders signal corresponding failure information
to the local multiplex controller that shall generate the MDT. After the failure
has been eliminated, the local uplink stops transmitting the MDT.
Details on the Multiplex Diagnostic Table concept can be found in Annex 1.
In addition it is recommended that a transmitted SERVICE DESCRIPTION TABLE (SDT)
includes the service information about all services on the respective
transponder on which it is transmitted, and that an EVENT INFORMATION TABLE
(EIT) includes the event information about all present and following events for
all services on the respective transponder.
6.6. SOURCE CODING
Source coding of video and audio signals shall conform to the following
specifications:
ISO/IEC 13818-2/-3
Generic coding of moving pictures and associated audio (Part 2: Video and
Part 3: Audio).
ETR 154
Digital broadcasting systems for television; Implementation guidelines for
the use of MPEG-2 systems; Video and audio in satellite and cable
broadcasting applications.
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7. ASTRA SATELLITE INFORMATION
7.1. ASTRA 1 SERIES
Presently, there are six ASTRA satellites (ASTRA 1A to 1F) at the orbital
position of 19.2 degrees East. In the middle of 1997, ASTRA 1G will be added to
fill the available frequency spectrum at 19.2 degrees East. ASTRA 1G is SES'
seventh satellite to be co-positioned at 19.2 degrees East. Adding 16
transponders, the spacecraft will increase the digital transmission capacity on
that position to 120 transponders.
The eight satellite at the 19.2 degrees East orbital position, ASTRA 1H will be
launched to provide backup capability for the other satellites at that position.
7.1.1. ASTRA 1 TRANSPONDER FREQUENCY PLAN
Figures 7.1.a. to 7.1.g. present the ASTRA 1 satellite system frequency plans.
All transponders are linearly polarised, utilising the polarisation scheme
presented in Table 7.1. The two polarisations are orthogonal to each other and
the horizontal polarisation has a counter-clockwise rotation of 7.5 degrees
relative to the orbit plane, as viewed from the satellite.
[Download Table]
TRANSPONDER UPLINK DOWNLINK
----------- ------ --------
Odd.................... Vertical Horizontal
Even................... Horizontal Vertical
Table 7.1 - ASTRA 1 TRANSPONDER POLARISATION SCHEME
All the ASTRA 1 satellites provide four different downlink coverage modes, as
detailed in Tables 7.1.a. to 7.1.b. These four modes provide different
coverage, concentrating more downlink power in different regions of Europe.
[Download Table]
SATELLITE ASTRA 1A ASTRA 1B ASTRA 1C ASTRA 1D
--------- -------- -------- -------- --------
MODE TRANSPONDER
-------- -------------------------------------------------------
Horizontal 1 1,5,9,13 17,21,25,29 33,37,41,45 49,53,57,61
Horizontal 2 3,7,11,15 19,23,27,31 35,39,43,47,63 51,55,59,63
Vertical 1 4,8,12,16 20,24,28,32 36,40,44,48,64 52,56,60,64
Vertical 2 2,6,10,14 18,22,26,30 34,38,42,46 50,54,58,62
TABLE 7.1.A. - ASTRA 1A TO 1D DOWNLINK
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[Enlarge/Download Table]
SATELLITE ASTRA 1E ASTRA 1F ASTRA 1G
MODE TRANSPONDER
Horizontal + ..... 65, 69, 73, 77, 81 85, 89, 93, 97, 101 105, 109, 113, 117
Horizontal - ..... 67, 71, 75, 79 83, 87, 91, 95, 99, 103 107, 111, 115, 119
Vertical - ....... 68, 72, 76, 80 84, 88, 92, 96, 100, 104 108, 112, 116, 120
Vertical + ....... 66, 70, 74, 78, 82 86, 90, 94, 98, 102 106, 110, 114, 118
Table 7.1.b. ASTRA 1E to 1G DOWNLINK
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[FIGURE 256]
Figure 7.1 a A-BAND FREQUENCY PLAN
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[FIGURE 257]
Figure 7.1 b B-BAND FREQUENCY PLAN
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[FIGURE 258]
Figure 7.1 c C-BAND FREQUENCY PLAN
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[FIGURE 259]
Figure 7.1 d D-BAND FREQUENCY PLAN
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[FIGURE 260]
Figure 7.1 e E-BAND FREQUENCY PLAN
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[FIGURE 261]
Figure 7.1 f F-BAND FREQUENCY PLAN
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[FIGURE 262]
Figure 7.1 g G-BAND FREQUENCY PLAN
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7.2. ASTRA 2 SERIES
As of autumn 1997, a second orbital position at 28.2 degrees East will be
activated with the deployment of ASTRA 2A. A second satellite, ASTRA 2B, will be
co-located at 28.2 degrees East in late 1998.
ASTRA 2A will have 28 active Ku-band transponders (32 for the first five years)
operating in the Broadcast Satellite Services frequency band (11.70 - 12.50
GHz), powered by 100 Watt travelling-wave tube amplifiers.
ASTRA 2B will provide up to 28 highpower Ku-band transponders (30 for the first
five years) with an output of 108 Watt each. All transponders can operate over
Europe and a steerable antenna offers the capability for up to 16 transponders
in the 12.50 - 12.75 GHz frequency range to be activated within any area of the
earth visible from 28.2 degrees East.
Co-located at 28.2 degrees East, the two spacecraft will provide SES with a
total of 56 transponders in the frequency range 11.70 - 12.75 GHz for digital
broadcasts at the second ASTRA orbital position.
7.2. ASTRA 2 TRANSPONDER FREQUENCY PLAN
Figures 7.2.a. and 7.2.b. present the ASTRA 2 satellite frequency plans. All
transponders are linearly polarised, utilising the polarisation scheme
presented in Table 7.2. The two polarisations are orthogonal to each other and
the horizontal polarisation has a counter-clockwise rotation of 7.5 degrees
relative to the orbit plane, as viewed from the satellite.
[Download Table]
Transponder Uplink Downlink
Odd................... Vertical Horizontal
Even.................. Horizontal Vertical
Table 7.2. - ASTRA 2 TRANSPONDER POLARISATION SCHEME
All the ASTRA 2 satellites provide different downlink coverage modes, as
detailed in Table 7.2.a. These four modes provide different coverage,
concentrating more downlink power in different regions of Europe.
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[Enlarge/Download Table]
SATELLITE ASTRA 2A ASTRA 2B
--------- ------------------------------ -----------------------------
TRANSPONDER
----------------------------------------------------------------------------------------------
Pol. Beam E-Band F-Band F-Band G-Band
----------------------------------------------------------------------------------------------
Horizontal ........ South 1, 5, 9, 13, 17 21, 25 29, 33, 37 41, 45, 49, 53
Horizontal ........ North 3, 7, 11, 15 19, 23, 27 31. 35. 39 43, 47, 51, 55
Vertical .......... South 2, 6, 10, 14, 18 22, 26, 30, 34, 38 42, 46, 50, 64
Vertical .......... North 4, 8, 12, 16 20, 24, 28 32, 36, 40 44, 48, 52, 56
Table 7.2.a. -- ASTRA 2A AND 2B DOWNLINK
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[FIGURE 265]
Figure 7.2 a ASTRA 2A FREQUENCY PLAN
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[FIGURE 266]
Figure 7.2 b ASTRA 2B Frequency Plan
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8. ORBITAL POSITION/STATION KEEPING
The nominal orbital position of the ASTRA 1 satellites is 19.2 degrees East. The
orbital position of the ASTRA 2 satellites is 28.2 degrees East.
Under normal operating conditions SES will maintain the ASTRA satellites within
the following station-keeping box:
+/- 0.10 degrees North/South
+/- 0.10 degrees East/West
9. BEACON INFORMATION
The following table shows the beacon frequencies (MHz) for the different
spacecraft:
[Download Table]
Vertical Horizontal
-------- ----------
ASTRA 1A.............. 11203.0 11446.5
ASTRA 1B............... 11453.5 11696.5
ASTRA 1C............... 11451.0 11448.5
ASTRA 1D............... 11454.0 11447.5
ASTRA 1E............... 11202.0 10948.5
ASTRA 1F............... 11201.0 10946.5
ASTRA 1G............... 11701.0 11699.0
ASTRA 1H............... 11707.0 11693.5
ASTRA 2A............... 11706.0 11694.5
ASTRA 2B............... 11708.0
11710.0
Table 9.1 BEACON FREQUENCIES (MHz)
At least one beacon will always be operational per spacecraft.
The beacon frequency stability is 1 ppm per day. Under normal operating
conditions the minimum beacon e.i.r.p. on any spacecraft shall be 16 dBW. For
the design of suitable tracking antenna systems, the following information
regarding the appropriate ASTRA ranging and telemetry characteristics shall be
used as a baseline.
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9.1 ASTRA 1A AND ASTRA 1B BEACON DETAILS
The following characteristics apply to both ASTRA 1A and ASTRA 1B.
PCM Telemetry : Phase modulation of beacon carrier by PCM (Biphase L)
telemetry to a peak deviation of 1.0+/-0.1 radians. Data
rate is 1 kbit/s.
Analog Telemetry : Phase modulation of beacon carrier by frequency modulated
14.5 kHz subcarrier to a peak deviation of 1.0+/-0.1
radians.
Ranging : Phase modulation of beacon carrier by ranging signals at
19 kHz or 27.777 kHz to a peak deviation of 1.0+/-0.1
radians.
Ranging + PCM
Telemetry : Phase modulation of beacon carrier by composite ranging
signals at 19 kHz or 27.777 kHz together with PCM telemetry
data signal to a peak deviation of 1.0+0.1 radians. In
absence of ranging signals, the deviation of PCM data alone
is 0.5+/-0.05 radians.
There are four ranging tones. The first three ranging tones at 35.43 Hz,
283.45 Hz and 3968.25 Hz serially frequency modulate the 19 kHz subcarrier.
The fourth ranging tone is at 27.777 kHz.
9.2. ASTRA 1C, 1D, 1E, 1F, 1G, 1H AND 2A BEACON DETAILS
The following characteristics apply to the beacons on ASTRA 1C, 1D, 1E, 1F,
1G, 1H and 2A.
During PCM-mode, the beacon is phase modulated (PM) by a telemetry subcarrier
with a subcarrier frequency of 32 kHz and a modulation index of 1.25+/-0.15
radians. The subcarrier is biphase modulated by telemetry data.
During ranging mode, the 32 kHz subcarrier is switched off and the beacon is
phase modulated by sequences of 4 ranging tones with a modulation index of
1.00+/-0.15 radians.
9.4. ASTRA 2B BEACON DETAILS
The following characteristics apply to the beacons on ASTRA 2B.
During PCM mode, the beacon is phase modulated (PM) by a telemetry
subcarrier with a subcarrier frequency of 32 kHz and a peak modulation index of
1.5 radians. The subcarrier is coherent PSK modulated by telemetry data.
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During ranging mode, the 32 kHz subcarrier is switched off and the
beacon is phase modulated by a ranging tone, which itself is modulated by
an ambiguity resolution code. The peak modulation index during ranging is
0.7 radians.
During simultaneous PCM and ranging on the TM downlink signal, the
PCM-modulated 32 kHz subcarrier and ranging tone are combined into one
baseband signal, which modulates the main carrier with max. effective
modulation indices of 1.4 radians for the PCM-signal and 0.4 radians for the
ranging tone.
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ANNEX 1
SOCIETE EUROPEENNE DES SATELLITES
TECHNICAL DEPARTMENT
MULTIPLEX DIAGNOSTIC TABLE (MDT)
1 INTRODUCTION
In a digital broadcast environment with a multitude of services there is a need
for highly automated means to monitor and subsequently to provide information
(e.g. failure messages) about the availability of services as well as of
service components such as video, audio and subtitling and of Service
information tables.
In order to support the detection of service failures, to provide information
for remedial measures and to efficiently log such events, a transport
mechanism, the Multiplex Diagnostic Table (MDT) has been defined. This system
will serve for conveying diagnostic information about the consistency of all
DVB/MPEG-2 multiplexes on ASTRA to the central Digital Network Operations
Centre (DINO) of Societe Europeenne des Satellites (SES).
2 FUNCTIONALITY
MDTs can be generated at any point in the transmission chain to signal missing
streams (e.g. video, audio, subtitle or accompanied data) or Service
Information components (e.g. NIT, SDT, EIT or TDT) within a multiplex. As the
underlying concept of the MDT system is to detect and signal failures at the
point where they are generated, the system supervisor of the DVB/MPEG-2
encoding, multiplexing and modulation equipment should monitor the correct
functioning of all equipment modules and should generate an MDT in the case a
service failure occurs for longer than 10 seconds.
MDTs shall then be periodically transmitted every 10 seconds until the failure
is fixed. In addition to faulty equipment modules also missing input streams
can be identified by subsequent modules in the transmission chain which then
generate corresponding MDTs.
This principle will be applied e.g. by the special monitor IRDs of the DINO
which can not only receive and extract incoming MDTs from the multiplexes but
also can generate MDTs in the case e.g. Service Information components are
missing. All MDTs are being fed via the ASTRA Service Information Update System
(ASIUS) into the Service Availability System (SAS) of the Digital Network
Operations Centre. Upon reception of an MDT an alert is initiated by the DINO
computer system which then enables the operator to act appropriately based on
detailed transponder specific diagnostic information provided together with the
alert message.
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3 SYNTAX OF THE MULTIPLEX DIAGNOSTIC TABLE (MDT)
The syntax of the MDT is conforming to the one defined in the standard ISO/IEC
13818-1 for the definition of private sections.
As defined in that standard, private data may be sent in transport stream
packets with PID not listed in the Program Map Table sections.
Therefore, Multiplex Diagnostic Tables shall be carried on PID 0x1FFD using the
normal payload unit start indicator/pointer field mechanism described in the
standard ISO/IEC 13818-1. This PID shall not be used for any other purpose on
the ASTRA Satellite Network. A MDT must be inserted in maximum one Transport
Stream Packet resulting in a maximum table size of 184 bytes.
multiplex diagnostic section()[
table id 8 uimsbf
section syntax indicator 1 bslbf
SES reserved 1 bslbf
ISO reserved 2 bslbf
section length 12 uimsbf
transport stream id 16 uimsbf
original network id 16 uimsbf
MDT version number 4 uimsbf
Fault source 12 uimsbf
Fault type 16 uimsbf
for (1=0;i<N;i++)[
Fault major 16 uimsbf
Fault minor 16 uimsbf
]
Table id = 0xB0
Section syntax indicator = 0
SES reserved = 1
Section length: This is a 12 bit field, the first two bits of which shall be
"00". It specifies the number of bytes of the section, starting immediately
following the section length field. The section length shall not exceed 181
bytes so that the entire section has a maximum length of 184 bytes.
Transport stream id: This is a 16 bit field which serves as a label to identify
the transport stream where the error or warning has occurred.
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ORIGINAL NETWORK ID: This 16 bit field gives the label identifying the
network id of the originating delivery system of the transport stream where the
error or warning has occured.
MDT VERSION NUMBER: This 4 bit field identifies the version number of the MDT
structure. Currently, the MDT version number shall be set to "0".
FAULT SOURCE: This is a code that, together with the transport stream id and
the original network id, identifies the origin of the failure. Fault source
values can be defined by the operator of the transport stream within the ranges
defined in Table 1.
FAULT TYPE: This 16 bit field identifies the basic type of errors or warnings.
Only values described in Table 2 are defined. In every MDT section only one
Fault type shall be listed resulting in only one basic type of error or warning
per MDT.
FAULT MAJOR: This 16 bit field provides more detailed information about the
errors or warnings as defined by the Fault type. Depending on the value of the
Fault type, the Fault major has different meanings. Currently, only the values
given in Table 4 and 5 are defined. If for a Fault type no Fault major code is
defined, the loop within the MDT shall be empty. If for a Fault type several
Fault major codes are defined the loop may contain more than one of these
codes. In case of missing components of a service (Fault type = 0x0100) the
Fault major code is equal to the service id of this service.
FAULT MINOR: This field provides additional information about the error or
warning as described by the combination of Fault type and Fault major. If no
Fault minor code is defined for a Fault major code, the Fault minor field shall
be present and all bits shall be set to "1". For the time being Fault minor is
only defined for Fault type = 0x0100 (Component of service missing) as
described in Table 3. In that case the service id of the service comprising the
missing component is defined in the Fault major field and the missing component
is defined in the Fault minor field.
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TABLE 1; FAULT SCORE
[Download Table]
--------------------------------------------------------------
Fault score range Description
--------------------------- ----------------------------
0x0000 Undefined
0x0001,...,0x0064 SI-editing & controller
0x0065,...,0x01F4 Audio encoder
0x01F5,...,0x0226 Video encoder
0x0227,...,0x03B6 Data inserter
0x03B7,...,0x03E8 CA system
0x03E9,...,0x041A Multiplexer
0x041B,...,0x044C Re-Multiplier
0x044D,...,0x047E Modulator
0x047F,...,0x060E Decoder
0x060F,...,0x0640 Network termination
0x0641,...,0x0A00 ASTRA reserved
0x0A01,...,0x0FFF User defined
TABLE 2: FAULT TYPE
[Download Table]
--------------------------------------------------------------
Fault type Description
--------------------------- ----------------------------
0x0000 Undefined
0x0001 NIT missing
0x0002 SDT missing
0x0004 EIT missing
0x0008 TDT missing
0x0009 PAT missing
0x000A CAT missing
0x0100 Component of service missing
Other fault type <= 0x0800 ASTRA reserved
Fault type > 0x0800 User defined
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Table 3: Fault minor codes for Fault type value = 0x0100 (COMPONENT MISSING)
(Fault major specifies the service id of the service missing components.)
[Download Table]
Fault minor
if Fault type = 0x0100 DESCRIPTION
---------------------- ------------------------------------
0x0001 Video component missing
0x0002 Audio component missing
0x0004 EBU Teletext subtitles missing
0x0008 Associated EBU Teletext missing
0x0010 Data component missing
0x0020 DVB subtitling missing
0x0040 PMT missing
Other values ASTRA reserved
Table 4: (Fault major codes for Fault type value = 0x0002 (SDT MISSING)
[Download Table]
Fault minor
if Fault type = 0x0002 (SDT MISSING) DESCRIPTION
------------------------------------ --------------------------------
0x0001 DVB-SI SDT missing
Other values ASTRA reserved
Table 5: Fault major codes for Fault type value = 0x0004 (EIT MISSING)
[Download Table]
Fault minor
if Faulttype = 0x0004 (EIT missing) DESCRIPTION
------------------------------------ --------------------------------
0x0001 DVB-SI EIT missing
Other values ASTRA reserved
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(ASTRA LOGO)
ASTRA SERVICE INFORMATION
UPDATE SYSTEM
(ASIUS)
TECHNICAL DESCRIPTION
SES - ASIUS CONFIDENTIAL
SYE - 045/12-96
06 December 1996
0
TABLE OF CONTENTS
1 INTRODUCTION ...................................................... 2
2 CONCEPT OF THE ASTRA SERVICE INFORMATION UPDATE SYSTEM ............ 2
3 FUNCTIONAL FEATURES OF ASUIS ...................................... 5
3.1 SI Data Structures considered by ASIUS........................ 5
3.1.1 Network Information Table (NIT)........................ 5
3.1.2 Service Description Table (SDT)........................ 5
3.1.3 Multiplex Diagnostic Table (MDT)....................... 9
3.2 SI Data Acquisition........................................... 9
3.3 SI Data Processing............................................ 10
3.4 SI Data Distribution.......................................... 10
4 GLOSSARY.................................... ...................... 12
5 REFERENCES......................................................... 13
ANNEX 1............................................................ 14
SES - ASIUS CONFIDENTIAL
SYE - 045/12-96
06 December 1996
1
1 INTRODUCTION
Service Information (SI) systems for Digital Video Broadcast are considered
by broadcasters and also by network operators as one of the crucial
elements in digital transmission of video, audio and data signals. With the
plethora of services being available in the digital age, an effective means
of guiding consumers around the various services on offer is an essential
pre-requisite of any consumer oriented digital transmission and reception
system. Beyond informing about the available services, there is also a need
to allow for the quick acquisition of any service that can be received.
Based on the DVB SI specification Societe Europeenne des Satellites (SES)
has developed the ASTRA Service Information Update System (ASIUS) for
providing tuning information and also for informing the digital IRDs about
all services on the ASTRA network. In addition ASIUS monitors the Service
Information on all transponders, checks the presence and the correctness of
this data and provides also diagnostics information on the consistency of
the multiplexes.
2 CONCEPT OF THE ASTRA SERVICE INFORMATION UPDATE SYSTEM
The ASTRA Service Information Update System (ASIUS) is an application of
the DVB Service Information specification as standardised in ETS 300468/1/
and may serve the Digital Satellite IRD to quickly tune to the receivable
services on ASTRA. It also enables the presentation of services and
broadcasters in a convenient way to the consumer.
This is achieved by compiling and transmitting an ASTRA Network
Information Table (ASTRA NIT) providing tuning information as well as an
ASTRA Service Description Table (ASTRA SDT) containing information about
all services on all transponders on the ASTRA network. Thus the IRD is
enabled to present the names of all services on ASTRA, the names of all
corresponding broadcasters (service providers) and the service types such
as TV, Radio, Teletext or data services, without having to tune to each
transponder.
The concept for the ASIUS involves the transmission of the ASTRA NIT on
each transponder. This NIT conveys information about the physical
parameters of all multiplexes on ASTRA (frequency, symbol rate, etc.) as
well as the information about the network itself (ID, name, satellite
position).
Furthermore, the concept involves the transmission of the ASTRA SDT on two
ASTRA Service Information channels (Barker Channels), one with horizontal
and one with vertical polarization.
SES - ASIUS CONFIDENTIAL
SYE - 045/12-96
06 December 1996
2
As it is the objective to provide up-to-date network information and service
description data about all transponders on ASTRA, a concept for an automatic
updating of the ASTRA NIT/SDT has been developed, considering all updates from
the Betzdorf earth station as well as the remote uplinks.
The ASTRA NIT is mainly under the administration of SES (network operator)
except for parts as e.g. the Forward Error Correction (FEC) scheme which may be
adjusted by the remote uplink operators.
The multiplex specific SDTs are under the administration of the broadcasters.
ASIUS receives the SDTs transmitted on all transponders, extracts those parts
directly related to each respective transponder and compiles an ASTRA SDT with
service description information (e.g. service names, service providers,
service types) about all services on ASTRA.
[FIGURE 278]
Figure 1: Transmission and updating of ASTRA NIT and SDT tables
SES - ASIUS CONFIDENTIAL
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3 FUNCTIONAL FEATURES OF ASIUS
3.1 SI DATA STRUCTURES CONSIDERED BY ASIUS
Regarding the various tables defined by MPEG-2 and by the DVB project, there are
only a few relevant for the ASIUS. These are the Network Information Table, the
Service Description Table, the Event Information Table (EIT), and the Time and
Date Table (TDT).
3.1.1 NETWORK INFORMATION TABLE (NIT)
The structure of the Network Information Table is presented in Figure 3. The
ASTRA NIT is divided in sections according to the MPEG-2 syntax. Each section
includes a loop over network related descriptors which is used for conveying the
networknamedescriptor and the linkagedescriptors to the ASTRA Service
Information channel.
For each transport stream the NIT contains a loop over transport stream related
descriptors including the satellitedeliverysystemdescriptor with information
such as frequency, polarisation, symbol rate and FEC scheme. Conveying an
optional servicelistdescriptor in that loop of the NIT is not considered by
ASIUS.
3.1.2 ASTRA SERVICE DESCRIPTION TABLE (SDT)
The structure of the Service Description Table is illustrated in Figure 4. The
ASTRA SDT is also divided into sections according to the MPEG-2 syntax. For each
Transport Stream at least one section with service description data is
transmitted. All SDT sections include a loop over all services on the
corresponding Transport Stream. For each service a loop of descriptors including
servicedescriptor and countryavailabilitydescriptor is conveyed.
NVODreferencedescriptor and timeshiftedservicedescriptor are also
considered by ASIUS. In order to identify the actual Transport Stream on which
Service Information is received and thus to identify the relevant SI parts that
have been updated at a remote uplink, the corresponding transportsstreamid can
be found in each header of a servicedescriptionsection for the actual
Transport Stream /1/.
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[FIGURE 280]
Figure 2: Interconnection between ASIUS and the Digital NOC
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[Download Table]
NETWORK INFORMATION TABLE (NIT)
ACTUAL NETWORK OTHER NETWORK
-------------- -------------
SECTION 1 SECTION 2 SECTION 3
--------- --------- ---------
network id
section number
FOR 1 = O ... N NETWORK DESCRIPTORS
network name descriptor
linkage descriptor
FOR 1 = O ... N TRANSPORT STREAMS
transport stream id
original network id
FOR 1 = O ... N TRANSPORT
DESCRIPTORS
delivery system descriptor
Figure 3: Structure of the Network Information Table
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[Download Table]
SERVICE DESCRIPTION TABLE (SDT)
OTHER
TRANSPORT
ACTUAL TRANSPORT STREAM STREAM
------------------------------------------------ ---------
TRANSPORT STREAM 1 TRANSPORT ...
STREAM 2
------------------------------------- --------- ----
SECTION 1 SECTION 2 SECTION 3
--------- --------- ---------
transport stream id
section number
original network id
FOR 1 = O ... N SERVICES
service id
scrambling yes/no
FOR 1 = O ... N DESCRIPTORS
service descriptor
country availability descriptor
NVOD reference descriptor
time shifted service descriptor
Figure 4: Structure of the Service Description Table
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3.1.3. MULTIPLEX DIAGNOSTIC TABLE (MDT)
In a digital broadcast environment with a multitude of services there is a need
for highly automated means to monitor and subsequently to provide information
(e.g. failure messages) about the availability of services as well as of service
components such as video, audio and subtitling and of Service Information
tables.
In order to support the detection of service failures, to provide information
for remedial measures and to efficiently log such events, a transport mechanism,
the Multiplex Diagnostic Table (MDT) has been defined by SES. This system is
serving for conveying diagnostic information about the consistency of all
DVB/MPEG-2 multiplexes on ASTRA to the central DINO in Betzdorf.
MDTs can be generated at any point in the transmission chain to signal missing
streams (e.g. video, audio, subtitle or accompanied data) or Service
Information components (e.g. NIT, SDT, EIT or TDT) within a multiplex. As the
underlying concept of the MDT system is to detect and signal failures at the
point where they are generated, the system supervisor of the DVB/MPEG-2
encoding, multiplexing and modulation equipment should monitor the correct
functioning of all equipment modules and should generate an MDT in the case a
service failure occurs for longer than 10 seconds.
MDTs shall then be periodically transmitted every 10 seconds until the failure
is fixed. In addition to faulty equipment modules also missing input streams
can be identified by subsequent modules in the transmission chain which then
generate corresponding MDTs.
This principle is applied e.g. by the special monitor IRDs of the DINO which
can not only receive an extract incoming MDTs from the multiplexes but also can
generate MDTs in the case e.g. Service Information components are missing. All
MDTs are being fed via the ASIUS into the Service Availability System (SAS) of
the Digital Network Operations Centre. Upon reception of an MDT an alert is
initiated by the DINO computer system which then enables the operator to act
appropriately based on detailed transponder specific diagnostic information
provided together with the alert message.
Details about the MDT concept can be found in Annex 1.
3.2. SI Data Acquisition
The ASTRA Service Information Update System in Betzdorf includes the reception
of all Transport Streams of the ASTRA Satellite System. From these Transport
Streams the relevant SI is extracted and passed over the ASIUS processing
station. This includes the NIT for the actual network (ASTRA) and the SDT for
the actual Transport Stream. If a MDT has been received (which occurs only in
case of a failure), it will also be transferred.
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to ASIUS.
The following processing steps have been implemented in ASIUS for the SI data
acquisition:
1. Reception of the DVB/MPEG-2 Transport Streams from all ASTRA transponders.
2. Extraction of all transponders SI data (NIT, MDT, SDT, EIT, TDT). By
means of the version number mechanism provided in each section syntax,
the IRD considers only the updated parts of this data.
3. Transmission of all the updates from the IRDs to ASIUS. The IRDs
furthermore monitor the availability of the NIT, SDT, EIT and TDT
(Time and Date Table) in each Transport Stream and shall generate a
Multiplex Diagnostic Table and transmit it to the ASIUS processor, if a
failure is detected.
3.3 SI DATA PROCESSING AND MONITORING
After having received an update the ASIUS compiles a new version of the
ASTRA NIT and ASTRA SDT. Since the system has immediate access to all
SI data on the ASTRA network it monitors the presence, correctness, and also
the consistency of the SI data. In case of an erroneous situation an alarm is
triggered and the operators in the DINO are informed.
3.4 SI DATA DISTRIBUTION
After the compilation of the received SI data by the ASIUS processor, the
updated ASTRA NIT is transmitted on all transponder uplinked from Betzdorf.
The ASTRA SDT is inserted into the two transponders which contain the ASTRA
Service Information channel. In addition a linkage descriptor is inserted in
the ASTRA NIT, which is available on all transponders. This descriptor points
to transport stream ids and service ids of the ASTRA Service Information
channels.
If the consumer wants to have access to the ASTRAL SDT the IRD will read the
linkage descriptor and tune to one of the corresponding transponders. After
the reading of the ASTRA SDT all services available on the ASTRA Satellite
System could be displayed. It is however assumed that certain filter
mechanisms would be applied to the data before displaying the information in a
consumer friendly way. More details on the functionality of the ASTRA Service
Information channel are described SES' "Technical Recommendations for Digital
IRDs"/2/. A flow chart of the access functionality for the ASTRA SDT is
depicted in Figure 5.
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06 December 1996 10
[FIGURE 285]
Figure 5: Example of the access functionality for the ASTRA SDT
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4 GLOSSARY
ASIUS ASTRA Service Information Update System
DNO Digital Network Operation Centre
DVB Digital Video Broadcasting
DTH Direct-to-Home satellite transmission
FEC Forward Error Correction
IRD Integrated Receiver Decoder
MDT Multiplex Diagnostic Table
NIT Network Information Table
NOC Network Operation Centre
NVOD Near-Video-On-Demand
SDT Service Description Table
SES Societe Europeenne des Satellites
SI Service Information
SMATV Satellite Master Antenna Television
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5 REFERENCES
/1/ ETS 300 468 "Digital broadcasting systems for television, sound and data
services; specification for Service Information (SI) in Digital Video
Broadcasting (DVB) Systems"
/2/ "Technical Recommendations for Digital Integrated Receiver Decoders", SES
SES-ASIUS CONFIDENTIAL
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06 December 1996
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ANNEX 1
SOCIETE EUROPEENNE DES SATELLITES
TECHNICAL DEPARTMENT
MULTIPLEX DIAGNOSTIC TABLE (MDT)
1 INTRODUCTION
In a digital broadcast environment with a multitude of services there is a need
for highly automated means to monitor and subsequently to provide information
(e.g. failure messages) about the availability of services as well as of service
components such as video, audio and subtitling and of Service Information
tables.
In order to support the detection of service failures, to provide information
for remedial measures and to efficiently log such events, a transport mechanism,
the Multiplex Diagnostic Table (MDT) has been defined. This system is serving
for conveying diagnostic information about the consistency of all DVB/MPEG-2
multiplexes on ASTRA to the central Digital Network Operations Centre (DINO) of
Societe Europeenne des Satellites (SES).
2 FUNCTIONALITY
MDTs can be generated at any point in the transmission chain to signal missing
streams (e.g. video, audio, subtitle or accompanied data) or Service Information
components (e.g. NIT, SDT, EIT or TDT) within a multiplex. As the underlying
concept of the MDT system is to detect and signal failures at the point where
they are generated, the system supervisor of the DVB/MPEG-2 encoding,
multiplexing and modulation equipment should monitor the correct functioning of
all equipment and should generate an MDT in the case a service failure occurs
for longer than 10 seconds.
MDTs shall then be periodically transmitted every 10 seconds until the failure
is fixed. In addition to faulty equipment modules also missing input streams
can be identified by subsequent modules in the transmission chain which then
generate corresponding MDTs.
This principle is applied e.g. by the special monitor IRDs of the DINO which can
not only receive and extract incoming MDTs from the multiplexes but also can
generate MDTs in the case e.g. Service Information components are missing. All
MDTs are being fed via the ASTRA Service Information Update System (ASIUS) into
the Service Availability System (SAS) of the Digital Network Operations Centre.
Upon reception of an MDT an alert is initiated by the DINO computer system which
then enables the operator to act
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appropriately based on detailed transponder specific diagnostic information
provided together with the alert message.
3 SYNTAX OF THE MULTIPLEX DIAGNOSTIC TABLE (MDT)
The syntax of the MDT is conforming to the one defined in the standard ISO/IEC
13818-1 for the definition of private sections.
As defined in that standard, private data may be sent in Transport Stream
packets with PID not listed in the Program Map Table sections.
Therefore, Multiplex Diagnostic Tables shall be carried on PID 0x1FFD using the
normal payload unit start indicator/pointer field mechanism described in the
standard ISO/IEC 13818-1. This PID shall not be used for any other purpose on
the ASTRA Satellite Network. A MDT must be inserted in maximum one Transport
Stream Packet resulting in a maximum table size of 184 bytes.
multiplex diagnostic section[
table id............................... 8 uimsbf
section syntax indicator............... 1 bslbf
SES reserved........................... 1 bslbf
ISO reserved........................... 2 bslbf
section length......................... 12 uimsbf
transport stream id.................... 16 uimsbf
original network id.................... 16 uimsbf
MDT version number..................... 4 uimsbf
Fault source........................... 12 uimsbf
Fault type............................. 16 uimsbf
for (l=0;i<N;i++)[
Fault major......................... 16 uimsbf
Fault minor......................... 16 uimsbf
]
TABLE ID = 0XB0
SECTION SYNTAX INDICATOR = 0
SES RESERVED = 1
SECTION LENGTH: this is a 12 bit field, the first two bits of which shall be
"00". it specifies the number of bytes of the section, starting immediately
following the section length field. the section length shall not exceed 181
bytes so that the entire section has a maximum length of 184 bytes.
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TRANSPORT STREAM ID: This is a 16 bit field which serves as a label to identify
the Transport Stream where the error or warning has occurred.
ORIGINAL NETWORK ID: This 16 bit field gives the label identifying the
networkid of the originating delivery system of the Transport Stream where the
error or warning has occurred.
MDT VERSION NUMBER: This 4 bit field identifies the version number of the MDT
structure. Currently, the MDT version number shall be set to "0".
FAULT SOURCE: This is a code that, together with transport stream id and the
original network id, identifies the origin of the failure. Fault source values
can be defined by the operator of the Transport Stream within the ranges
defined in Table 1.
FAMILY TYPE: This 16 bit field identifies the basic type of errors or warnings.
Only values described in Table 2 are defined. In every MDT section only one
Fault type shall be listed resulting in only one basic type of error or warning
per MDT.
FAULT MAJOR: This 16 bit field provides more detailed information about the
errors or warnings as defined by the Fault type. Depending on the value of the
Fault type, the Fault major has different meanings. Currently, only the values
given in Table 4 and 5 are defined. If for a Fault type no Fault major code is
defined, the loop within the MDT shall be empty. If for a Fault type several
Fault major codes are defined the loop may contain more than one of these
codes. In case of missing components of a service (Fault type = 0x0100) the
Fault major code is equal the service id of this service.
FAULT MINOR: This field provides additional information about the error or
warning as described by the combination of Fault type and Fault major. If no
Fault minor code is defined for a Fault major code, the Fault minor field shall
be present and all bits shall be set to "1". For the time being Fault minor is
only defined for Fault type = 0x0100 (Component of service missing) as
described in Table 3. In that case the service id of the service comprising
the missing component is defined in the Fault major field and the missing
component is defined in the Fault minor field.
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TABLE 1: FAULT SOURCE
[Download Table]
Fault source range Description
------------------------------- ----------------------------
0x0000 Undefined
0x0001,...,0x0064 SI-editing & controlled
0x0065,...,0x01F4 Audio encoder
0x01F5,...,0x0226 Video encoder
0x0227,...,0x03B6 Data inserter
0x03B7,...,0x03E8 CA system
0x03E9,...,0x041A Multiplexer
0x041B,...,0x044C Re-multiplexer
0x044D,...,0x047E Modulator
0x047F,...,0x060E Decoder
0x060F,...,0x0640 Network termination
0x0641,...,0x0A00 ASTRA reserved
0x0A01,...,0x0FFF User defined
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TABLE 2: FAULT TYPE
[Download Table]
Fault type Description
----------------------------- ---------------------------
0x0000 Undefined
0x0001 NIT missing
0x0002 SDT missing
0x0004 EIT missing
0x0008 TDT missing
0x0009 PAT missing
0x000A CAT missing
0x0010 Component of service missing
Other fault type <= 0x0800 ASTRA reserved
Fault type > 0x0800 User defined
Table 3: Fault minor codes for Fault type value = 0x0100 (COMPONENT MISSING)
(Fault major specifies the service id of the service with missing components)
[Download Table]
Fault minor Description
if Fault type = 0x0100
----------------------------- ------------------------------
0x0001 Video component missing
0x0002 Audio component missing
0x0004 EBU Teletext subtitles missing
0x0008 Associated EBU Teletext missing
0x0010 Data component missing
0x0020 DVB subtitling missing
0x0040 PMT missing
Other values ASTRA reserved
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TABLE 4: FAULT MAJOR CODES FOR FAULT TYPE VALUE = 0x0002 (SDT MISSING)
[Download Table]
Fault major
if Fault type = 0x0002 (SDT missing) Description
------------------------------------ ------------------------
0x0001 DVB-SI SDT missing
Other values ASTRA reserved
TABLE 5: FAULT MAJOR CODES FOR FAULT TYPE VALUE = 0x0004 (EIT MISSING)
[Download Table]
Fault major
if Fault type = 0x0004 (EIT missing) Description
------------------------------------ ------------------------
0x0001 DVB-SI EIT missing
Other values ASTRA reserved
The information and data contained herein are subject to change.
Societe Europeenne des Satellites S.A.
L-6815 Chateau de Betzdorf, Luxembourg
Tel.: (352) 71 07 25-1, Fax: (352) 71 07 25-548
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15 DECEMBER 1995
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