Attachment Sched S Tech Report

This document pretains to SAT-LOA-20100726-00167 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2010072600167_832692

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: INTELSAT 17 1/19/2011 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 7/28/2008 16.2 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 10/21/2010 49 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: 11/15/2010 2/15/2011 2674 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 Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode f. 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) 5850 M 6425 M R Fixed Satellite Service 3625 M 4200 M T Fixed Satellite Service 13750 M 14500 M R Fixed Satellite Service 10950 M 11200 M T Fixed Satellite Service 11450 M 11700 M T Fixed Satellite Service 12500 M 12750 M T 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: 66 E REPLACE INTELSAT 702 Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be N/S Station-Keeping provided (Optional): 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 (o) Other Plane (Seconds) Node (Deg.) (Degrees) Angle 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) 1 S AFRICA, EUROPE, WEST ASIA, INDIA 2 S EUROPE, AFRICA, ASIA, AUSTRALIA 3 S GLOBAL 4 S EUROPE, RUSSIA, NORTHERN CHINA 5 S NORTHERN AFRICA, EUROPE, MIDDLE EAST 6 S MID AND SOUTHERN AFRICA

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) (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB) ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Input Output Max. System Max. Saturation (Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step (dBi) (dBi) Losses Power (W) EIRP Noice Gain Pt. Flux Density (Y/N) Value Size (dB) (dBW) Temp (k) (db/K) (dBW/m2) HAU R 27 21 0.16 0.16 30 N 1 645 -1.1 -103.5 24 1 HBU R 27 21 0.16 0.16 30 N 1 645 -1.1 -103.5 24 1 LMU R 26.4 16.4 0.16 0.16 22 N 90 2 660 -1.8 -100.2 24 1 LMU R 26.4 16.4 0.16 0.16 23 N 02 660 -1.8 -100.2 24 1 GAU R 20.6 16.6 0.16 0.16 30 N 3 692 -7.8 -97 24 1 GBU R 20.6 16.6 0.16 0.16 30 N 3 692 -7.8 -97 24 1 RUU R 34 28 0.16 0.16 30 N 90 4 630 6 -102.6 22 1 EMU R 33.2 25.2 0.16 0.16 28.5 N 0 5 630 5.2 -103.7 22 1 AFU R 34.8 28.8 0.16 0.16 30 N 90 6 645 6.7 -99.8 22 1 GSU R 35 31 0.16 0.16 30 N 90 3 676 6.7 -103.5 22 1 HAD T 25.2 21.2 0.16 0.16 30 N 1 3.5 28.8 39.8 HBD T 25.2 21.2 0.16 0.16 30 N 1 3.5 28.8 39.8 LMD T 24.6 16.6 0.16 0.16 25 N 02 3.5 28.8 39.2 LMD T 24.6 16.6 0.16 0.16 25 N 90 2 3.5 28.8 39.2 GAD T 20.6 16.6 0.16 0.16 30 N 3 2.2 38.9 36.5 GBD T 20.6 16.6 0.16 0.16 30 N 3 2.2 38.9 36.5 RUD T 33.5 27.5 0.16 0.16 30 N 04 2 95.5 53.3 EMD T 32.5 26.5 0.16 0.16 28.5 N 90 5 3.4 69.2 50.9 AFD T 33.6 27.6 0.16 0.16 30 N 06 3.3 70.8 52.1 GSD T 33.4 29.4 0.16 0.16 30 N 03 2 95.5 53.2 CMD R 20.6 16.6 0.16 0.16 N 3 18724 -22.1 -110.2 CMD R 2 -1 0.16 0.16 N 3 4813 -34.8 -97.5 CMD R 6 3 0.16 0.16 N 3 27064 -38.3 -94 TLM T 20.6 16.6 0.16 0.16 N 3 6.1 0.2 13.5 TLM T 13.2 10.2 0.16 0.16 N 3 5.3 13.3 13.2 TLM T 6 3 0.16 0.16 N 3 10 3.1 10.9 UPC T 20.5 17.5 0.16 0.16 N 03 4.2 0.15 12.3 UPC T 20.5 17.5 0.16 0.16 N 90 3 4.2 0.15 12.3 UPK T 22.9 15.9 0.16 0.16 N 3 5.1 0.31 17.8

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) HAU R C 66 haul.gxt HBU R C 66 hbur.gxt LMU R C 66 lmuv.gxt LMU R C 66 lmuh.gxt GAU R C 66 gaul.gxt GBU R C 66 gbur.gxt RUU R C 66 ruuv.gxt EMU R C 66 emuh.gxt AFU R C 66 afuv.gxt GSU R C 66 gsuv.gxt HAD T C 66 hadr.gxt -153.5 -153.4 -153.2 -153.1 -153 HBD T C 66 hbdl.gxt -153.5 -153.4 -153.2 -153.1 -153 LMD T C 66 lmdh.gxt -154.1 -154 -153.8 -153.7 -153.6 LMD T C 66 lmdv.gxt -154.1 -154 -153.8 -153.7 -153.6 GAD T C 66 gadr.gxt -156.8 -156.7 -156.5 -156.4 -156.3 GBD T C 66 gbdl.gxt -156.8 -156.7 -156.5 -156.4 -156.3 RUD T C 66 rudh.gxt -148 -145.5 -143 -140.5 -139.5 EMD T C 66 emdv.gxt -148 -145.5 -143 -142 -141.9 AFD T C 66 afdh.gxt -148 -145.5 -143 -140.8 -140.7 GSD T C 66 gsdh.gxt -150 -147.5 -145 -142.5 -140 CMD R C 66 cmdc.gxt CMD R C 66 cmdw.pdf CMD R C 66 cmdm.pdf TLM T C 66 tlmc.gxt -167.7 -167.6 -167.5 -167.4 -167.3 TLM T C 66 tlmw.pdf -168 -167.9 -167.8 -167.7 -167.6 TLM T C 66 tlmm.pdf -170.3 -170.2 -170.1 -170 -169.9 UPC T C 66 upch.pdf -158.9 -158.8 -158.7 -158.6 -158.5 UPC T C 66 upcv.pdf -158.9 -158.8 -158.7 -158.6 -158.5

UPK T C 66 upkr.pdf -153.4 -153.3 -153.2 -153.1 -153 LMU R X 66 luvx.pdf LMU R X 66 luhx.pdf EMU R X 66 euhx.pdf LMD T X 66 lhdx.pdf LMD T X 66 lhdx.pdf EMD T X 66 edvx.pdf

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 ID Gain (dB) No. ID No. (T or C) AALU 72000 R 5890 L C AHR 128 AALU HAUL AARD HADR BBLU 72000 R 5970 L C BHR 128 BBLU HAUL BBRD HADR 3LU 36000 R 6030 L C 3HR 128 3LU HAUL 3RD HADR 4VU 36000 R 6070 V C 4LH 125.6 4VU LMUV 4HD LMDH 5VU 36000 R 6110 V C 5LH 125.6 5VU LMUV 5HD LMDH 6VU 36000 R 6150 V C 6LH 125.6 6VU LMUV 6HD LMDH 7VU 36000 R 6200 V C 7LH 125.6 7VU LMUV 7HD LMDH 8VU 36000 R 6240 V C 8LH 125.6 8VU LMUV 8HD LMDH 9LU 36000 R 6280 L C 9GA 129.8 9LU GAUL 9RD GADR 10LU 36000 R 6320 L C 10GA 129.8 10LU GAUL 10RD GADR 11LU 36000 R 6360 L C 11GA 129.8 11LU GAUL 11RD GADR 12LU 41000 R 6402.5 L C 12GA 129.8 12LU GAUL 12RD GADR AARU 72000 R 5890 R C AHL 128 AARU HBUR AALD HBDL BBRU 72000 R 5970 R C BHL 128 BBRU HBUR BBLD HBDL 3RU 36000 R 6030 R C 3HL 128 3RU HBUR 3LD HBDL 4HU 36000 R 6070 H C 4LV 125.6 4HU LMUH 4VD LMDV 5HU 36000 R 6110 H C 5LV 125.6 5HU LMUH 5VD LMDV 6HU 36000 R 6150 H C 6LV 125.6 6HU LMUH 6VD LMDV 7HU 36000 R 6200 H C 7LV 125.6 7HU LMUH 7VD LMDV 8HU 36000 R 6240 H C 8LV 125.6 8HU LMUH 8VD LMDV 9RU 36000 R 6280 R C 9GB 129.8 9RU GBUR 9LD GBDL 10RU 36000 R 6320 R C 10GB 129.8 10RU GBUR 10LD GBDL 11RU 36000 R 6360 R C 11GB 129.8 11RU GBUR 11LD GBDL 12RU 36000 R 6402.5 R C 12GB 129.8 12RU GBUR 12LD GBDL AARD 72000 T 3665 R C 4RR 132.8 4RVU RUUV 4RHD RUDH BBRD 72000 T 3745 R C 5RR 132.8 5RVU RUUV 5RHD RUDH 3RD 36000 T 3805 R C 6RR 132.8 6RVU RUUV 6RHD RUDH 4HD 36000 T 3845 H C 7RR 132.8 7RVU RUUV 7RHD RUDH 5HD 36000 T 3885 H C 8RR 132.8 8RVU RUUV 8RHD RUDH 6HD 36000 T 3925 H C 1RR 132.8 1RVU RUUV 1RHD RUDH

7HD 36000 T 3975 H C 2RR 132.8 2RVU RUUV 2RHD RUDH 8HD 36000 T 4015 H C 3RR 132.8 3RVU RUUV 3RHD RUDH 9RD 36000 T 4055 R C 4MM 133.3 4MHU EMUH 4MVD EMDV 10RD 36000 T 4095 R C 5MM 133.3 5MHU EMUH 5MVD EMDV 11RD 36000 T 4135 R C 6MM 133.3 6MHU EMUH 6MVD EMDV 12RD 41000 T 4177.5 R C 7MM 133.3 7MHU EMUH 7MVD EMDV AALD 72000 T 3665 L C 8MM 133.3 8MHU EMUH 8MVD EMDV BBLD 72000 T 3745 L C AMM 133.3 AMHU EMUH AMVD EMDV 3LD 36000 T 3805 L C BMM 133.3 BMHU EMUH BMVD EMDV 4VD 36000 T 3845 V C 1MM 133.3 1MHU EMUH 1MVD EMDV 5VD 36000 T 3885 V C 2MM 133.3 2MHU EMUH 2MVD EMDV 6VD 36000 T 3925 V C 3MM 133.3 3MHU EMUH 3MVD EMDV 7VD 36000 T 3975 V C 4AA 127.9 4AVU AFUV 4AHD AFDH 8VD 36000 T 4015 V C 5AA 127.9 5AVU AFUV 5AHD AFDH 9LD 36000 T 4055 L C 6AA 127.9 6AVU AFUV 6AHD AFDH 10LD 36000 T 4095 L C 7AA 127.9 7AVU AFUV 7AHD AFDH 11LD 36000 T 4135 L C 8AA 127.9 8AVU AFUV 8AHD AFDH 12LD 41000 T 4177.5 L C 1AA 127.9 1AVU AFUV 1AHD AFDH 1RVU 72000 R 13795 V C 2AA 127.9 2AVU AFUV 2AHD AFDH 2RVU 72000 R 13875 V C 3AA 127.9 3AVU AFUV 3AHD AFDH 3RVU 72000 R 13955 V C ASS 133.3 ASVU GSUV ASHD GSDH 4RVU 72000 R 14045 V C BSS 133.3 BSVU GSUV BSHD GSDH 5RVU 72000 R 14125 V C AMS 134.7 AMHU EMUH ASHD GSDH 6RVU 72000 R 14205 V C BMS 134.7 BMHU EMUH BSHD GSDH 7RVU 72000 R 14295 V C 1RA 131.5 1RVU RUUV 1AHD AFDH 8RVU 72000 R 14375 V C 2RA 131.5 2RVU RUUV 2AHD AFDH 1MHU 72000 R 13795 H C 3RA 131.5 3RVU RUUV 3AHD AFDH 2MHU 72000 R 13875 H C 1AR 129.2 1AVU AFUV 1RHD RUDH 3MHU 72000 R 13955 H C 2AR 129.2 2AVU AFUV 2RHD RUDH 4MHU 72000 R 14045 H C 3AR 129.2 3AVU AFUV 3RHD RUDH 5MHU 72000 R 14125 H C ASM 131.6 ASVU GSUV AMVD EMDV 6MHU 72000 R 14205 H C BSM 131.6 ASVU GSUV BMVD EMDV 7MHU 72000 R 14295 H C 8MHU 72000 R 14375 H C AMHU 36000 R 14440 H C BMHU 36000 R 14480 H C 1AVU 72000 R 13795 V C 2AVU 72000 R 13875 V C 3AVU 72000 R 13955 V C

4AVU 72000 R 14045 V C 5AVU 72000 R 14125 V C 6AVU 72000 R 14205 V C 7AVU 72000 R 14295 V C 8AVU 72000 R 14375 V C ASVU 36000 R 14440 V C BSVU 36000 R 14480 V C 4RHD 72000 T 10995 H C 5RHD 72000 T 11075 H C 6RHD 72000 T 11155 H C 7RHD 72000 T 11495 H C 8RHD 72000 T 11575 H C 1RHD 72000 T 12547 H C 2RHD 72000 T 12627 H C 3RHD 72000 T 12707 H C 4MVD 72000 T 10995 V C 5MVD 72000 T 11075 V C 6MVD 72000 T 11155 V C 7MVD 72000 T 11495 V C 8MVD 72000 T 11575 V C AMVD 36000 T 11640 V C BMVD 36000 T 11680 V C 1MVD 72000 T 12547 V C 2MVD 72000 T 12627 V C 3MVD 72000 T 12707 V C 4AHD 72000 T 10995 H C 5AHD 72000 T 11075 H C 6AHD 72000 T 11155 H C 7AHD 72000 T 11495 H C 8AHD 72000 T 11575 H C 1AHD 72000 T 12547 H C 2AHD 72000 T 12627 H C 3AHD 72000 T 12707 H C ASHD 36000 T 11640 H C BSHD 36000 T 11680 H C CMD1 1000 R 6173.7 L T CMD2 1000 R 6176.3 L T CMD3 1000 R 6173.7 L T CMD4 1000 R 6176.3 L T

CMD5 1000 R 6173.7 L T CMD6 1000 R 6176.3 L T TLM1 500 T 3947.5 R T TLM2 500 T 3952.5 R T TLM3 500 T 3947.5 R T TLM4 500 T 3952.5 R T TLM5 500 T 3947.5 R T TLM6 500 T 3952.5 R T UPC1 25 T 3950 H T UPC2 25 T 3950.5 V T UPC3 25 T 11198 R T UPC4 25 T 11452 R T UPC5 25 T 12502 R 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) D1 72M0G7W 72000 4 49138 0.5 3.4 17.9 D2 41M0G7W 41000 4 27981 0.5 3.4 13.2 D3 36M0G7W 36000 4 24575 0.5 3.4 18.1 D4 10M3G7W 10300 4 6000 0.5 3.9 16.9 D5 100KG7W 100 4 64 0.5 3 16.9 D6 1M45G7W 1450 2 512 0.5 3.4 14.7 D7 400KG7W 400 2 128 0.5 3.4 14.1

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) A1 36M0F3F 36000 TV/FM 1 PAL 16.6 1.5 10 24.3

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. (o)Assoc. Transponder (kHz) No.) Bandwidth (Table (Table S12) Stn. Max. Power (dBW) Power Flux Stn (a) Start (b) End (kHz) S11) Antenna Density Rec. G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dBW/m2/Hz) (dB/K) AHR BSM A1 2 36000 IS17 SCHEDUL 4000 54.1 18.3 24.3 31.6 35.6 -156.5 28.4 AHR BSM D1 1 72000 NOTE.txt 52.8 16.6 22.6 35.8 39.8 -164.1 19.2 AHR BSM D4 4 10300 NOTE.txt 51 12.4 18.4 25.5 29.5 -164.9 19.2 AHR BSM D5 521 100 NOTE.txt 51 -8 -2 5.1 9.1 -165.8 19.2 AHR BSM A1 1 36000 NOTE.txt 4000 58.4 14.3 24.3 31.2 39.2 -152.9 31 AHR BSM D3 1 36000 NOTE.txt 54.1 14.6 24.6 31.2 39.2 -161.7 19.2 AHR BSM D4 3 10300 NOTE.txt 54.1 13.9 23.9 22.2 30.2 -164.2 21 AHR BSM D5 237 100 NOTE.txt 54.1 -4.4 5.6 3.9 11.9 -163 19.2 AHR BSM A1 1 36000 NOTE.txt 4000 55.4 19.5 23.5 32.5 36.5 -155.6 26.2 AHR BSM D2 1 41000 NOTE.txt 51 17.9 21.9 32.5 36.5 -165 19.2 AHR BSM D4 2 10300 NOTE.txt 51 17.4 21.4 24.7 28.7 -165.7 19.2 AHR BSM D5 295 100 NOTE.txt 51 -3 1 4.3 8.3 -166.6 19.2 AHR BSM A1 2 36000 NOTE.txt 4000 56.9 11.9 17.9 39.3 45.3 -146.8 33.1 AHR BSM D1 1 72000 NOTE.txt 56.9 18.6 24.6 45.8 51.8 -152.1 18.8 AHR BSM D4 5 10300 NOTE.txt 56.9 -4.8 1.2 35.2 41.2 -153.2 22.3 AHR BSM D5 541 100 NOTE.txt 56.9 -25.1 -19.1 14.9 20.9 -154 22.3 AHR BSM D6 34 1450 NOTE.txt 56.9 -13.1 -7.1 26.9 32.9 -154.1 22.3 AHR BSM D7 180 400 NOTE.txt 46.4 -7.7 -1.7 11.8 17.8 -163.2 33.1 AHR BSM A1 2 36000 NOTE.txt 4000 56.9 14.7 20.7 39.3 45.3 -146.8 33.1 AHR BSM D1 1 72000 NOTE.txt 56.9 17.4 23.4 45.8 51.8 -152.1 22.3 AHR BSM D4 5 10300 NOTE.txt 56.9 -3.2 2.8 34.7 40.7 -153.7 22.3 AHR BSM D5 593 100 NOTE.txt 56.9 -23.4 -17.4 14.5 20.5 -154.4 22.3 AHR BSM D6 37 1450 NOTE.txt 56.9 -11.4 -5.4 26.5 32.5 -154.5 22.3 AHR BSM D7 180 400 NOTE.txt 46.4 -11 -5 16.4 22.4 -158.6 33.1 AHR BSM A1 2 36000 NOTE.txt 4000 56.9 17.5 23.5 41.3 47.3 -144.8 31 AHR BSM D1 1 72000 NOTE.txt 56.9 17.3 23.3 45.8 51.8 -152.1 22.3 AHR BSM D4 5 10300 NOTE.txt 56.9 2 8 34 40 -154.4 22.3 AHR BSM D5 536 100 NOTE.txt 56.9 -18.3 -12.3 13.7 19.7 -155.2 22.3 AHR BSM D6 33 1450 NOTE.txt 56.9 -6.3 -0.3 25.7 31.7 -155.3 22.3

AHR BSM D7 180 400 NOTE.txt 46.4 -8.5 -2.5 13 19 -162 33.1 AHR BSM A1 2 36000 NOTE.txt 4000 56.9 17.7 23.7 41.3 47.3 -144.8 28.6 AHR BSM D1 1 72000 NOTE.txt 56.9 17.5 23.5 45.8 51.8 -152.1 22.3 AHR BSM D4 5 10300 NOTE.txt 56.9 -0.8 5.2 34 40 -154.4 22.3 AHR BSM D5 534 100 NOTE.txt 56.9 -21.1 -15.1 13.7 19.7 -155.2 22.3 AHR BSM D6 33 1450 NOTE.txt 56.9 -9.1 -3.1 25.8 31.8 -155.2 22.3 AHR BSM D7 180 400 NOTE.txt 46.4 -9.3 -3.3 15 21 -160 33.1 AHR BSM A1 2 36000 NOTE.txt 4000 56.9 12.5 20.5 38.3 44.3 -147.8 34.6 AHR BSM D1 1 72000 NOTE.txt 56.9 15.3 23.3 44.9 50.9 -153 22.3 AHR BSM D4 5 10300 NOTE.txt 56.9 -2.1 5.9 32.6 38.6 -155.8 25 AHR BSM D5 554 100 NOTE.txt 56.9 -22.3 -14.3 12.4 18.4 -156.5 25 AHR BSM D6 34 1450 NOTE.txt 56.9 -10.3 -2.3 24.4 30.4 -156.6 25 AHR BSM D7 180 400 NOTE.txt 49 -11.5 -3.5 15.3 21.3 -159.7 33.1 AHR BSM A1 2 36000 NOTE.txt 4000 56.9 12.7 16.7 38.3 44.3 -147.8 34.6 AHR BSM D3 1 36000 NOTE.txt 56.9 16.8 20.8 42.8 48.8 -152.1 22.3 AHR BSM D4 2 10300 NOTE.txt 56.9 -3.7 0.3 35.8 41.8 -152.6 22.3 AHR BSM D5 266 100 NOTE.txt 56.9 -24 -20 15.6 21.6 -153.3 22.3 AHR BSM D6 16 1450 NOTE.txt 56.9 -12 -8 27.6 33.6 -153.4 22.3 AHR BSM D7 90 400 NOTE.txt 46.4 -10.3 -6.3 18.7 24.7 -156.3 33.1 AHR BSM A1 1 36000 NOTE.txt 4000 56.9 18.2 22.2 48 52 -140.1 25 AHR BSM D3 1 36000 NOTE.txt 56.9 14.2 18.2 44.8 48.8 -152.1 18.8 AHR BSM D4 3 10300 NOTE.txt 56.9 -1.5 2.5 38.4 42.4 -152 18.8 AHR BSM D5 360 100 NOTE.txt 56.9 -21.7 -17.7 18.1 22.1 -152.8 18.8 AHR BSM D6 24 1450 NOTE.txt 56.9 -9.7 -5.7 30.1 34.1 -152.9 18.8 AHR BSM D7 90 400 NOTE.txt 42.9 -6.5 -2.5 19.3 23.3 -157.7 33.1 AHR BSM A1 1 36000 NOTE.txt 4000 56.9 18 26 48 52 -140.1 25 AHR BSM D3 1 36000 NOTE.txt 56.9 14 22 44.8 48.8 -152.1 18.8 AHR BSM D4 3 10300 NOTE.txt 56.9 0.2 8.2 38.2 42.2 -152.2 18.8 AHR BSM D5 360 100 NOTE.txt 56.9 -20.1 -12.1 17.9 21.9 -153 18.8 AHR BSM D6 24 1450 NOTE.txt 56.9 -8.1 -0.1 29.9 33.9 -153.1 18.8 AHR BSM D7 90 400 NOTE.txt 42.9 -5.4 2.6 18.6 22.6 -158.4 33.1

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: 3400 INTERNATIONAL DRIVE, N.W. S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: WASHINGTON DC 20008 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 202-944-7701

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 2466 (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: 5612 26.1 0.921 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1072 9.2 0.845 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 74.3 7.7 0.778 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): 8752 8752 8752 8752 Bus (Watts): (b): (g): (l): (q): 2459 1192 2459 1192 Total (Watts): (c): (h): (m): (r): 11211 9944 11211 9944 Solar Array (Watts): (d): (i): (n): (s): 12405 11328 12216 11155 Depth of Battery (e) (j) (o) (t) Discharge (%): 58.8 % % 62.7 % % 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: 2010-08-03 10:57:48
Document Modified: 2010-08-03 10:57:48
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