Attachment Sched S Tech Report

This document pretains to SAT-LOA-20121002-00172 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2012100200172_971231

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: SES-129K N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 24 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: 864 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) 14.00 G 14.50 G R Fixed Satellite Service 11.70 G 12.20 G T Fixed Satellite Service 11.70 G 12.20 G T 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: 129.1 W Avoids overlapping with the stationkeeping boxes of Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Ciel-2 and Galaxy-12, also located at the nominal 129 N/S Station-Keeping provided (Optional): W orbit location d. Toward West: Degrees E/W 0.05 Degrees Tolerance: g. Westernmost: e. Toward East: 0.05 Degrees 0.05 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) K-DL E CONUS, Alaska, Hawaii, Mexico and parts of Canada and the Caribbean. K-UL E CONUS, Alaska, Hawaii, Mexico and parts of Canada and the Caribbean

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) KRH R 35 25 0.15 0 30 Y 0 K-UL 550 7.6 -101.6 21 1 KRV R 35 25 0.15 0 30 Y 90 K-UL 550 7.6 -101.6 21 1 KTH T 33.5 23.5 0.15 0 30 Y 0 K-DL 3.5 134 54.8 KTV T 33.5 23.5 0.15 0 30 Y 90 K-DL 3.5 134 54.8 KTR T 33.5 23.5 0.15 0 30 Y K-DL 3.5 134 54.8 KTL T 33.5 23.5 0.15 0 30 Y K-DL 3.5 134 54.8

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) KRH R C -129.1 krh.gxt KRV R C -129.1 krv.gxt KTH T C -129.1 kth.gxt KTV T C -129.1 ktv.gxt KTR T C -129.1 ktr.gxt KTL T C -129.1 ktl.gxt

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) KR01 36000 R 14020 H C K01 119.5 KR01 KRH KT01 KTV KR02 36000 R 14040 V C K03 119.5 KR03 KRH KT03 KTV KR03 36000 R 14060 H C K05 119.5 KR05 KRH KT05 KTV KR04 36000 R 14080 V C K07 119.5 KR07 KRH KT07 KTV KR05 36000 R 14100 H C K09 119.5 KR09 KRH KT09 KTV KR06 36000 R 14120 V C K11 119.5 KR11 KRH KT11 KTV KR07 36000 R 14140 H C K13 119.5 KR13 KRH KT13 KTV KR08 36000 R 14160 V C K15 119.5 KR15 KRH KT15 KTV KR09 36000 R 14180 H C K17 119.5 KR17 KRH KT17 KTV KR10 36000 R 14200 V C K19 119.5 KR19 KRH KT19 KTV KR11 36000 R 14220 H C K21 119.5 KR21 KRH KT21 KTV KR12 36000 R 14240 V C K23 119.5 KR23 KRH KT23 KTV KR13 36000 R 14260 H C K02 119.5 KR02 KRV KT02 KTH KR14 36000 R 14280 V C K04 119.5 KR04 KRV KT04 KTH KR15 36000 R 14300 H C K06 119.5 KR06 KRV KT06 KTH KR16 36000 R 14320 V C K08 119.5 KR08 KRV KT08 KTH KR17 36000 R 14340 H C K10 119.5 KR10 KRV KT10 KTH KR18 36000 R 14360 V C K12 119.5 KR12 KRV KT12 KTH KR19 36000 R 14380 H C K14 119.5 KR14 KRV KT14 KTH KR20 36000 R 14400 V C K16 119.5 KR16 KRV KT16 KTH KR21 36000 R 14420 H C K18 119.5 KR18 KRV KT18 KTH KR22 36000 R 14440 V C K20 119.5 KR20 KRV KT20 KTH KR23 36000 R 14460 H C K22 119.5 KR22 KRV KT22 KTH KR24 36000 R 14480 V C K24 119.5 KR24 KRV KT24 KTH KT01 36000 T 11720 V C TBC1 KBCC1 KTL KT02 36000 T 11740 H C TBC2 KBCC2 KTR KT03 36000 T 11760 V C K25 119.5 KR01 KRH KT25 KTR KT04 36000 T 11780 H C K26 119.5 KR02 KRV KT26 KTL KT05 36000 T 11800 V C K27 119.5 KR03 KRH KT27 KTR KT06 36000 T 11820 H C K28 119.5 KR04 KRV KT28 KTL

KT07 36000 T 11840 V C K29 119.5 KR05 KRH KT29 KTR KT08 36000 T 11860 H C K30 119.5 KR06 KRV KT30 KTL KT09 36000 T 11880 V C K31 119.5 KR07 KRH KT31 KTR KT10 36000 T 11900 H C K32 119.5 KR08 KRV KT32 KTL KT11 36000 T 11920 V C K33 119.5 KR09 KRH KT33 KTR KT12 36000 T 11940 H C K34 119.5 KR10 KRV KT34 KTL KT13 36000 T 11960 V C K35 119.5 KR11 KRH KT35 KTR KT14 36000 T 11980 H C K36 119.5 KR12 KRV KT36 KTL KT15 36000 T 12000 V C K37 119.5 KR13 KRH KT37 KTR KT16 36000 T 12020 H C K38 119.5 KR14 KRV KT38 KTL KT17 36000 T 12040 V C K39 119.5 KR15 KRH KT39 KTR KT18 36000 T 12060 H C K40 119.5 KR16 KRV KT40 KTL KT19 36000 T 12080 V C K41 119.5 KR17 KRH KT41 KTR KT20 36000 T 12100 H C K42 119.5 KR18 KRV KT42 KTL KT21 36000 T 12120 V C K43 119.5 KR19 KRH KT43 KTR KT22 36000 T 12140 H C TCK KUC1 KRH KT23 36000 T 12160 V C TBK1 KBCN1 KTH KT24 36000 T 12180 H C TBK2 KBCN2 KTV KT25 36000 T 11720 R C K44 119.5 KR20 KRV KT44 KTL KT26 36000 T 11740 L C K45 119.5 KR21 KRH KT45 KTR KBCC1 400 T 11701 L T K46 119.5 KR22 KRV KT46 KTL KBCC2 400 T 12199 R T K47 119.5 KR23 KRH KT47 KTR KT27 36000 T 11760 R C K48 119.5 KR24 KRV KT48 KTL KT28 36000 T 11780 L C KT29 36000 T 11800 R C KT30 36000 T 11820 L C KT31 36000 T 11840 R C KT32 36000 T 11860 L C KT33 36000 T 11880 R C KT34 36000 T 11900 L C KT35 36000 T 11920 R C KT36 36000 T 11940 L C KT37 36000 T 11960 R C KT38 36000 T 11980 L C KT39 36000 T 12000 R C KT40 36000 T 12020 L C KT41 36000 T 12040 R C KT42 36000 T 12060 L C KT43 36000 T 12080 R C

KT44 36000 T 12100 L C KT45 36000 T 12120 R C KT46 36000 T 12140 L C KT47 36000 T 12160 R C KT48 36000 T 12180 L C KUC1 800 R 14499 H T KBCN1 400 T 11701 H T KBCN2 400 T 12199 V 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) K_A 36M0G7W 36000 4 40000 0.69 6.4 19 K_B 27M0G7W 27000 4 32000 0.69 6.4 19 K_C 6M95G1W 6950 4 8000 0.69 6.4 19 K_D 5M00G1W 5000 4 6000 0.69 6.4 19 K_E 100KG1W 100 4 56 0.69 6.4 19 K_F 1M60G1W 1600 4 1544 0.69 6.4 19 K_G 36M0G7W 36000 8 50000 0.61 9.9 20

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) K_H 36M0F3F 36000 TV/FM 1 NTSC 12.8 1.29 11 20 K_TC 800KF9D 800 10 20 K_TM 400KF9D 400 10 20

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) K01 K48 K_A 1 link budgets r1. 57.3 20 25 44.8 54.8 -146.7 20.9 K01 K48 K_B 1 link budgets r1. 57.3 20 25 43.6 53.6 -146.7 20.9 K01 K48 K_C 5 6950 link budgets r1. 53 8.9 14 34.7 44.7 -149.7 26.9 K01 K48 K_D 6 5000 link budgets r1. 53 8.9 14 33.2 43.2 -149.7 26.9 K01 K48 K_E 250 100 link budgets r1. 46.7 -2 3 16.2 26.2 -149.7 20.9 K01 K48 K_F 20 1544 link budgets r1. 46.7 8 13 28.3 38.3 -149.7 26.9 K01 K48 K_G 1 link budgets r1. 57.3 20 25 44.8 54.8 -146.7 26.9 K01 K48 K_H 1 link budgets r1. 2000 57.3 22 25 44.8 54.8 -134.2 20.9 TCK TCK K_TC 1 link budgets r1. 60.2 10 15 TBK1 TBC2 K_TM 1 link budgets r1. 10 27 -155 34.6

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): #Error Remote Control (TT C) Location(s): S14a: Street Address: Woodbine TT&C S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Mt. Airy MD 21771 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 410-549-4300 E7169 Remote Control (TT C) Location(s): S14a: Street Address: Vernon Valley Spacecraft Operations S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Sussex NJ 07461 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 973-823-6000 WB81

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 2346 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3146 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5492 32.4 0.932 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1248.6 7.3 0.88 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 32.4 7 0.823 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): 13853 13853 13853 13853 Bus (Watts): (b): (g): (l): (q): 3265 1730 3265 1730 Total (Watts): (c): (h): (m): (r): 17118 15583 17118 15583 Solar Array (Watts): (d): (i): (n): (s): 21209 19010 19079 17286 Depth of Battery (e) (j) (o) (t) Discharge (%): 69.2 % 69.2 % 69.2 % 69.2 % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: YES NO X 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: 2012-10-16 13:42:33
Document Modified: 2012-10-16 13:42:33
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