Attachment Sched S Tech Report

This document pretains to SAT-MOD-20120524-00087 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2012052400087_954468

FCC 312 FEDERAL COMMUNICATIONS COMMISSION Page 1: General, Schedule S SATELLITE SPACE STATION AUTHORIZATIONS Frequency Bands, (Technical and Operational Description) and GSO Orbit S1. GENERAL INFORMATION Complete for all satellite applications. a. Space Station or Satellite Network Name: e. Estimated Date of Placement into Service: i Will the space station(s) operate on a Common Carrier Basis: AMC-2 3/5/1997 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 1/1/1994 17.5 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 8/1/1996 48 0 MHz d1. Est Launch Date Begin: d2. Est Launch Date End: h. Total Transponder Bandwidth (no. transponders x Bandwidth) l. Orbit Type: Mark all boxes that apply: 1/30/1997 1/30/1997 1920 MHz GSO NGSO X S2. OPERATING FREQUENCY BANDS Identify the frequency range and transmit/receive mode for all frequency bands in which this station will oper Also indicate the nature of service(s) for each frequency band. Frequency Band Limits f. Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode Nature of Service(s): List all that apply to this band a. Numeric b. Unit c. Numeric d. Unit (K/M/G) (K/M/G) 14.0 G 14.5 G R Fixed Satellite Service 11.7 G 12.2 G T Direct to Home in the Fixed Fixed Satellite Service 11.7 G 12.20 G T Fixed Satellite Service 5.925 G 6.425 G R Fixed Satellite Service 3.7 G 4.2 G T Fixed Satellite Service 14.0 G 14.5 G R Direct to Home in the Fixed Fixed Satellite Service S3. ORBITAL INFORMATION FOR GEOSTATIONARY SATELLITES ONLY: a. Nominal Orbital Longitude (Degrees E/W): b. Alternate Orbital Longitude (Degrees E/W): c. Reason for orbital location selection: 19 E Redeploy AMC-2 to the nominal 19.2E orbit location Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be (specifically at 19.0E) where it can introduce new N/S Station-Keeping provided (Optional): service in the Ku-band frequencies. d. Toward West: Degrees E/W 0.1 Degrees Tolerance: g. Westernmost: e. Toward East: 0.1 Degrees Degrees h. Easternmost: i. Reason for service are selection (Optional):

FEDERAL COMMUNICATIONS COMMISSION Page 2: NGSO Orbits SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S4. ORBITAL INFORMATION FOR NON-GEOSTATIONARY SATELLITES ONLY S4a. Total Number of Satellites in Network or System: S4c. Celestial Reference Body (Earth, Sun, Moon, etc.): S4b. Total Number of Orbital Planes in Network or System: S4d. Orbit Epoch Date: For each Orbital Plane Provide: (e) Orbital (f) No. of (g) Inclination (h) Orbital (i) Apogee (km) (j) Perigee (km) (k) Right Ascension (l) Argument of Active Service Arc Range (Degrees) Plane No. Satellites in Angle (degrees) Period of the Ascending Perigee (m) Begin (n) End Angle (o) Other Plane (Seconds) Node (Deg.) (Degrees) Angle S5. INITIAL SATELLITE PHASE ANGLE For each satellite in each orbital plane, provide the intital phase angle. (a) Orbital (b) Satellite (c) Initial Plane No. Number Phase Angle (Degrees) NO NGSO DATA FILED

FEDERAL COMMUNICATIONS COMMISSION Page 3: Service Areas SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S6. SERVICE AREA CHARACTERISTICS for each service area provide: (a) Service Area (b) Type of Associated (c) Service Area Diagram (d) Service Area Description. Provide list of geographic areas (state postal codes or ITU 3-ltr codes), satellites or Figure No. of ID Station (Earth or File Name (GXT File) Service Area Diagram. Space) KUL S Southern Africa KDL S Southern Africa CUL S Southern Africa CDL S Southern Africa GBL S Global region for TT&C

FEDERAL COMMUNICATIONS COMMISSION Page 4: Antenna Beams SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S7. SPACE STATION ANTENNA BEAM CHARACTERISTICS For each antenna beam provide: (a) (b) Isotropic Antenna (e) (f) (g) Min. (h) Polar- (i) Polarization (j) Service Transmit Receive Beam T/R Gain Pointing Rotational Cross- ization Alignment Rel. Area ID (k) Input (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB) ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Losses Output Max. System Max. Saturation (Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step (dBi) (dBi) (dB) Power (W) EIRP Noice Gain Pt. Flux Density (Y/N) Value Size (dBW) Temp (k) (db/K) (dBW/m2) KRV R 30.86 24.86 0.15 0 30 Y 90 KUL 550 3.46 -96.5 18 1 KRH R 33.63 27.63 0.15 0 30 Y 0 KUL 590 5.93 -99 18 1 KTV T 33 27 0.15 0 30 Y 90 KDL 1.5 41.7 49.2 KTH T 33.27 27.27 0.15 0 30 Y 0 KDL 1.4 43.7 49.68 CRV R 31.3 25.3 0.15 0 30 Y 90 CUL 531 4.05 -101.1 18 1 CRH R 32.89 26.89 0.15 0 30 Y 0 CUL 510 5.82 -103 18 1 CTV T 31.04 25.04 0.15 0 30 Y 90 CDL 1.9 12.8 42.1 CTH T 30.31 24.31 0.15 0 30 Y 0 CDL 2.5 11.2 40.8 GBL R 0 0.15 0 30 Y 90 GBL 600 -7 GBLT T 0 0.15 0 30 Y 90 GBL 12

FEDERAL COMMUNICATIONS COMMISSION Page 5: Beam Diagrams SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S8. ANTENNA BEAM DIAGRAMS For each beam pattern provide the reference to the graphic image and numerical data: Also provide the power flux density levels in each beam that result from the emission with the highest power flux density. (a) (b) (c) Co-or (d) GSO (e) NGSO Antenna Gain (f) GSO Antenna Max. Power Flux Density (dBW/M2/Hz) Beam T/R Cross Ref. Contour Description Gain Contour Data At Angle of Arrival above horizontal (for emission with highest PFD) ID Mode Polar Orbital (Figure/Table/ Exhibit) (GXT File) (g) 5 Deg (h) 10 Deg (i) 15 Deg (j) 20 Deg (k) 25 Deg Mode ("C" Longitude or" X") (Deg. E/W) KRV R C 19 AMC-2 KRVedit.gxt KRH R C 19 AMC-2 KRHedit.gxt CRV R C 19 AMC-2 CRVedit.gxt CRH R C 19 AMC-2 CRHedit.gxt KTV T C 19 AMC-2 KTVedit.gxt KTH T C 19 AMC-2 KTHedit.gxt CTV T C 19 AMC-2 CTVedit.gxt -174.84 -173.72 -172.62 -172 -170.4 CTH T C 19 AMC-2 CTHedit.gxt -173.34 -172.52 -172.12 -170.6 -168.6

FEDERAL COMMUNICATIONS COMMISSION Page 6: Channels and SATELLITE SPACE STATION AUTHORIZATIONS Transponders FCC Form 312 - Schedule S: (Technical and Operational Description) S9. SPACE STATION CHANNELS For each frequency channel provide: S10. SPACE STATION TRANSPONDERS For each transponder provide: (a) (B) Assigned (c) (d) Center (e) (f) TTC (a) (b) Receive Band Transmit Band Channel Bandwidth T/R Frequency Polarization or Comm Transponder Transponder (c) Channel (d) Beam (e) Channel (f) Beam ID No. (kHz) Mode (MHz) (H, V, L, R) Channel (T ID Gain (dB) No. ID No. or C) KR001 36000 R 14020 V C K0001 120 KR001 KRV KT001 KTH KR002 36000 R 14040 H C K0002 120 KR002 KRH KT002 KTV KR003 36000 R 14060 V C K0003 120 KR003 KRV KT003 KTH KR004 36000 R 14080 H C K0004 120 KR004 KRH KT004 KTV KR005 36000 R 14100 V C K0005 120 KR005 KRV KT005 KTH KR006 36000 R 14120 H C K0006 120 KR006 KRH KT006 KTV KR007 36000 R 14140 V C K0007 120 KR007 KRV KT007 KTH KR008 36000 R 14160 H C K0008 120 KR008 KRH KT008 KTV KR009 36000 R 14180 V C K0009 120 KR009 KRV KT009 KTH KR010 36000 R 14200 H C K0010 120 KR010 KRH KT010 KTV KR011 36000 R 14220 V C K0011 120 KR011 KRV KT011 KTH KR012 36000 R 14240 H C K0012 120 KR012 KRH KT012 KTV KR013 36000 R 14260 V C K0013 120 KR013 KRV KT013 KTH KR014 36000 R 14280 H C K0014 120 KR014 KRH KT014 KTV KR015 36000 R 14300 V C K0015 120 KR015 KRV KT015 KTH KR016 36000 R 14320 H C K0016 120 KR016 KRH KT016 KTV KR017 36000 R 14340 V C K0017 120 KR017 KRV KT017 KTH KR018 36000 R 14360 H C K0018 120 KR018 KRH KT018 KTV KR019 36000 R 14380 V C K0019 120 KR019 KRV KT019 KTH KR020 36000 R 14400 H C K0020 120 KR020 KRH KT020 KTV KR021 36000 R 14420 V C K0021 120 KR021 KRV KT021 KTH KR022 36000 R 14440 H C K0022 120 KR022 KRH KT022 KTV KR023 36000 R 14460 V C K0023 120 KR023 KRV KT023 KTH KR024 36000 R 14480 H C K0024 120 KR024 KRH KT024 KTV KT001 36000 T 11720 H C C0001 109 CR001 CRH CT001 CTV KT002 36000 T 11740 V C C0002 109 CR002 CRV CT002 CTH KT003 36000 T 11760 H C C0003 109 CR003 CRH CT003 CTV KT004 36000 T 11780 V C C0004 109 CR004 CRV CT004 CTH KT005 36000 T 11800 H C C0005 109 CR005 CRH CT005 CTV KT006 36000 T 11820 V C C0006 109 CR006 CRV CT006 CTH

KT007 36000 T 11840 H C C0007 109 CR007 CRH CT007 CTV KT008 36000 T 11860 V C C0008 109 CR008 CRV CT008 CTH KT009 36000 T 11880 H C C0009 109 CR009 CRH CT009 CTV KT010 36000 T 11900 V C C0010 109 CR010 CRV CT010 CTH KT011 36000 T 11920 H C C0011 109 CR011 CRH CT011 CTV KT012 36000 T 11940 V C C0012 109 CR012 CRV CT012 CTH KT013 36000 T 11960 H C C0013 109 CR013 CRH CT013 CTV KT014 36000 T 11980 V C C0014 109 CR014 CRV CT014 CTH KT015 36000 T 12000 H C C0015 109 CR015 CRH CT015 CTV KT016 36000 T 12020 V C C0016 109 CR016 CRV CT016 CTH KT017 36000 T 12040 H C C0017 109 CR017 CRH CT017 CTV KT018 36000 T 12060 V C C0018 109 CR018 CRV CT018 CTH KT019 36000 T 12080 H C C0019 109 CR019 CRH CT019 CTV KT020 36000 T 12100 V C C0020 109 CR020 CRV CT020 CTH KT021 36000 T 12120 H C C0021 109 CR021 CRH CT021 CTV KT022 36000 T 12140 V C C0022 109 CR022 CRV CT022 CTH KT023 36000 T 12160 H C C0023 109 CR023 CRH CT023 CTV KT024 36000 T 12180 V C C0024 109 CR024 CRV CT024 CTH CR001 36000 R 5945 H C C1 TC GBLRV CR002 36000 R 5965 V C T1 TM1 GBLTV CR003 36000 R 5985 H C T2 TM2 GBLTV CR004 36000 R 6005 V C T3 TM3 KTH CR005 36000 R 6025 H C CR006 36000 R 6045 V C CR007 36000 R 6065 H C CR008 36000 R 6085 V C CR009 36000 R 6105 H C CR010 36000 R 6125 V C CR011 36000 R 6145 H C CR012 36000 R 6165 V C CR013 36000 R 6185 H C CR014 36000 R 6205 V C CR015 36000 R 6225 H C CR016 36000 R 6245 V C CR017 36000 R 6265 H C CR018 36000 R 6285 V C CR019 36000 R 6305 H C CR020 36000 R 6325 V C CR021 36000 R 6345 H C

CR022 36000 R 6365 V C CR023 36000 R 6385 H C CR024 36000 R 6405 V C CT001 36000 T 3720 V C CT002 36000 T 3740 H C CT003 36000 T 3760 V C CT004 36000 T 3780 H C CT005 36000 T 3800 V C CT006 36000 T 3820 H C CT007 36000 T 3840 V C CT008 36000 T 3860 H C CT009 36000 T 3880 V C CT010 36000 T 3900 H C CT011 36000 T 3920 V C CT012 36000 T 3940 H C CT013 36000 T 3960 V C CT014 36000 T 3980 H C CT015 36000 T 4000 V C CT016 36000 T 4020 H C CT017 36000 T 4040 V C CT018 36000 T 4060 H C CT019 36000 T 4080 V C CT020 36000 T 4100 H C CT021 36000 T 4120 V C CT022 36000 T 4140 H C CT023 36000 T 4160 H C CT024 36000 T 4180 V C TC 800 R 6423.5 V T TM1 300 T 3700.5 V T TM2 300 T 4199.5 V T TM3 300 T 12198.0 H T

FEDERAL COMMUNICATIONS COMMISSION Page 7: Digital Modulation SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S11. DIGITAL MODULATION PARAMETERS For each digital emission provide: (a) Digital (b) Emission (c) Assigned (d) No. of (e)Uncoded (f) FEC Error (g) CDMA (h) Total C/N (i) Single Entry Mod. ID Designator Bandwidth Phases Data Rate Correction Processing Performance C/I Objective (kHz) (kbps) Coding Rate Gain (dB) Objective (dB) (dB) KU_1 6M95G7W 6945 4 8000 0.69 6.9 19.1 KU_2 5M00G1W 5035 4 5800 0.69 6.9 19.1 KU_3 100KG1W 55 4 56 0.69 6.9 19.1 KU_4 1M60G7W 1390 4 1544 0.75 9.3 21.5 C_1 9M00G7W 9000 4 6144 0.46 4.1 16.3 C_2 1M50G7W 1508 4 1544 0.69 6.9 19.1 C_3 100KG1D 55 4 56 0.67 6.9 19.1 C_4 4M05G7W 4050 4 2765 0.46 4.1 16.3 KU_5 36M0G7W 36000 4 48350 0.81 6.9 19.1

FEDERAL COMMUNICATIONS COMMISSION Page 8: Analog Modulation SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S12. ANALOG MODULATION PARAMETERS For each analog emission provide: (a) (b) Emission (c) (d) Signal (e) Multi-channel Telephony (j) Video (k) Video (l) Video (m) SCPC/FM (n) Total C/N (o) Single Analog Designator Assigned Type Channels Standard Noise- and Compander, Performance Entry C/I (f) Ave. (g) Bottom (h) Top (i) RMS Mod. ID Bandwidth per Carrier NTSC, Weighting SCPC/FM Preemphasis, Objective Objective Companded Baseband Baseband Modulation (kHz) PAL, etc. (dB) Modulation and Noise (dB) (dB) Talker Level Freq. (MHz) Freq. (MHz) Index Index Weighting (dB) (dBm0) Q_C 800KF9D 800 1 10 21 R_C 300KF9D 300 1 9 21 S_KU 300KF9D 300 1 9 21

FEDERAL COMMUNICATIONS COMMISSION Page 9: Typical Emissions SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S13. TYPICAL EMISSIONS For each planned type of emission provide: Associated Modulation ID (e) Carriers (f) Carrier (g)Noise Budget (h) Energy Receive Band (Assoc. Transmit Stn) Transmit Band (This Space Station) Transponder ID Range per Spacing Reference (Table Dispersal (c) Digital (d) Analog (i)Assoc. Assoc. Station Transmit EIRP (dBW) (n) Max. Power (o)Assoc. Transponder (kHz) No.) Bandwidth (Table S11) (Table S12) Stn. Max. Power (dBW) Flux Density Stn Rec. (a) Start (b) End (kHz) Antenna (dBW/m2/Hz) G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dB/K) K0001 K0024 KU_1 4 9000 Ku_Link_Budge 49.1 6.6 12.5 35.6 38.5 -155.6 26.9 K0001 K0024 KU_2 6 6000 Ku_Link_Budge 49.1 5.2 11.1 34.2 37.1 -155.6 26.9 K0001 K0024 KU_3 360 100 Ku_Link_Budge 49.1 -14.9 6.6 14 16.9 -155.6 26.9 K0001 K0024 KU_4 23 1566 Ku_Link_Budge 53.1 -4.4 1.5 28.7 31.6 -155.1 30.9 C1 C1 Q_C 1 Telecommand_ 55.6 29.8 32.8 T1 T2 R_C 1 Telemetry_Link 0 3 -162.3 33 T3 T3 S_KU 1 Telemetry_Link 9 12 -164.7 38.3 K0001 K0024 KU_5 1 KU_Link Budge 49.1 14.1 20 41.6 49.68 -151.8 26.9

FEDERAL COMMUNICATIONS COMMISSION Page 10: TT and C SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S14. Is the space station(s) controlled and monitored remotely? If Yes, provide the location and telephone number of the TT and C control point(s): Yes Remote Control (TT C) Location(s): S14a: Street Address: SES Engineering S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Betzdorf L-6815 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): +352 710 725 1 Remote Control (TT C) Location(s): S14a: Street Address: Nemea Earth Station S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Nemea 20500 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): +30 210 8252 692

FEDERAL COMMUNICATIONS COMMISSION Page 11: SATELLITE SPACE STATION AUTHORIZATIONS Characteristics and FCC Form 312 - Schedule S: (Technical and Operational Description) Certifications S15. SPACECRAFT PHYSICAL CHARACTERISTICS: S15a: Mass of spacecraft without fuel (kg): Spacecraft Dimensions Probability of Survival to 1310.8 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1338.3 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2649 26.8 0.78 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 320 1.8 0.88 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 75.5 3.78 0.69 S16. SPACECRAFT ELECTRICAL CHARACTERISTICS: Spacecraft Electrical Power (Watts) At Electrical Power (Watts) At Subsystem Beginning of Life End of Life At Equinox At Solstice At Equinox At Solstice Payload (Watts): (a): (f): (k): (p): 3772 3740 3772 3740 Bus (Watts): (b): (g): (l): (q): 1089 674 1089 674 Total (Watts): (c): (h): (m): (r): 4861 4414 4861 4414 Solar Array (Watts): (d): (i): (n): (s): 6513 6212 5250 4836 Depth of Battery (e) (j) (o) (t) Discharge (%): 70 % 70 % 70 % 70 % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: X YES NO N/A b. Are the appropriate service area coverage requirements of § 25.143(b)(ii) and (iii), or § 25.145(c)(1) and (2) met? YES NO X N/A c. Are the frequency tolerances of § 25.202(e) and the out-of-band emission limits of § 25.202(f)(1), (2) and (3) met? X YES NO N/A In addition to the information required in this Form, the space station applicant is required to provide all the information specified in Section 25.114 of the Commission's rules, 47 C.F.R § 25.114.


Document Created: 2012-06-11 10:20:59
Document Modified: 2012-06-11 10:20:59
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