Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20090410-00043 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2009041000043_707352

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 15 2/28/2010 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 3/28/2007 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 4/30/2009 22 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: 10/1/2009 12/31/2009 1304 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) 10950 M 11200 M T Fixed Satellite Service 11450 M 11700 M T Fixed Satellite Service 12500 M 12750 M T Fixed Satellite Service 13750 M 14000 M R Fixed Satellite Service 14000 M 14500 M R 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: 85.15 E TO REPLACE INTELSAT 709 CURRENTLY Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be OPERATING AT 85.15E 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 MIDDLE EAST AND NORTH AFRICA 2 S RUSSIA 3 S EAST ASIA 4 S GLOBAL

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) MEH R 36.5 28.5 0.14 0.12 N 01 713 8 -123.9 36 1 MEV R 37.4 27.4 0.14 0.12 N 90 1 700 9 -122.8 36 1 RUH R 33.5 27.5 0.14 0.12 N 0 2 590 5.8 -120.1 36 1 EIVU R 29.8 23.8 0.14 0.12 N 90 3 542 2.5 -124.2 36 1 WIV R 30.7 24.7 0.14 0.12 N 90 1 501 3.7 -124.4 36 1 MEH T 36.3 28.3 0.14 0.12 N 0 1 2.8 79.4 55.3 MEV T 37 29 0.14 0.12 N 90 1 3.4 58.9 54.7 RUV T 34.2 28.2 0.14 0.12 N 90 2 3.3 60.3 52 EIHD T 28.2 22.2 0.14 0.12 N 0 3 3.1 74.1 46.9 WIH T 31.1 25.1 0.14 0.12 N 0 1 2.6 83.2 50.3 CMH R 21.3 13.3 0.14 0.12 N 04 29676 -23.4 -103.9 CML R 13.8 12.8 0.14 0.12 N 4 21999 -29.6 -97.7 CML R 2.7 -0.8 0.14 0.12 N 4 14204 -38.8 -88.5 TUV T 22.4 17.6 0.14 0.12 N 90 4 2.7 0.4 18.1 TMV T 22.4 17.6 0.14 0.12 N 90 4 0.8 0.6 20.5 TMR T 13.4 12.4 0.14 0.12 N 4 11.8 0.8 12.5 TMR T 2.7 -0.8 0.14 0.12 N 4 6.6 1.9 5.4 UPH T 22.4 19.8 0.14 0.12 N 04 3.7 0.3 17.7 UPV T 22.4 19.8 0.14 0.12 N 90 4 3.7 0.3 17.7

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) MEH R C 85.15 MEHU.gxt MEV R C 85.15 MEVU.gxt RUH R C 85.15 RUHU.gxt EIVU R C 85.15 EIVU.gxt WIV R C 85.15 WIVU.gxt MEH T C 85.15 MEHD.gxt -150 -147.5 -145 -142.5 -140 MEV T C 85.15 MEVD.gxt -148 -145.5 -143 -140.5 -138.1 RUV T C 85.15 RUVD.gxt -148 -145.5 -143 -140.9 -140.8 EIHD T C 85.15 EIHD.gxt -148 -146.3 -146.1 -146 -145.9 WIH T C 85.15 WIHD.gxt -148 -145.5 -143 -142.6 -142.5 CMH R C 85.15 cmhg.gxt CML R C 85.15 cmlw.gxt CML R C 85.15 cmlo.pdf TUV T C 85.15 tuvg.gxt -163.9 -163.8 -163.7 -163.6 -163.5 TMV T C 85.15 tmvg.gxt -161.5 -161.4 -161.3 -161.2 -161.1 TMR T C 85.15 tmrw.gxt -169.5 -169.4 -169.3 -169.2 -169.1 TMR T C 85.15 tmro.pdf -176.6 -176.5 -176.4 -176.3 -176.2 UPH T C 85.15 uphg.gxt -153.5 -153.4 -153.3 -153.2 -153.1 UPV T C 85.15 upvg.gxt -153.5 -153.4 -153.3 -153.2 -153.1

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) 1KU 72000 R 13795 H C 1K 149.5 1KU MEHU 1KD MEVD 3KU 72000 R 13875 H C 3K 149.5 3KU MEHU 3KD MEVD 5KU 72000 R 13955 H C 5K 149.5 5KU MEHU 5KD MEVD 7KU 36000 R 14030 H C 7KMM 149.5 7KU MEHU 7KD MEVD 9KU 36000 R 14070 H C 7KMR 149.6 7KU MEHU 7KD RUVD 11KU 36000 R 14110 H C 9KMM 149.5 9KU MEHU 9KD MEVD 13KU 36000 R 14150 H C 9KMR 149.6 9KU MEHU 9KD RUVD 15KU 36000 R 14190 H C 11KMM 149.5 11KU MEHU 11KD MEVD 17KU 36000 R 14230 H C 11KMR 149.6 11KU MEHU 11KD RUVD 19KU 72000 R 14295 H C 13KMM 149.5 13KU MEHU 13KD MEVD 21KU 72000 R 14375 H C 13KMR 149.6 13KU MEHU 13KD RUVD 23KU 72000 R 14455 H C 15KMM 149.5 15KU MEHU 15KD MEVD 2KU 72000 R 13795 V C 15KMR 149.6 15KU MEHU 15KD RUVD 4KU 72000 R 13875 V C 17KMM 149.5 17KU MEHU 17KD MEVD 6KU 72000 R 13955 V C 17KMR 149.6 17KU MEHU 17KD RUVD 18KU 112000 R 14315 V C 19K 149.5 19KU MEHU 19KD MEVD 20KU 112000 R 14435 V C 21K 149.5 21KU MEHU 21KD MEVD 8KU 72000 R 14048 V C 23K 149.5 23KU MEHU 23KD MEVD 10KU 36000 R 14110 V C 2K 148.8 2KU MEVU 2KD MEHD 12KU 36000 R 14150 V C 4K 148.8 4KU MEVU 4KD MEHD 14KU 36000 R 14190 V C 6K 148.8 6KU MEVU 6KD MEHD 16KU 36000 R 14190 V C 18K 148.8 18KU MEVU 18KD MEHD 1KD 72000 T 10995 V C 20K 148.8 20KU MEVU 20KD MEHD 3KD 72000 T 11075 V C 7KRR 148.8 7KU RUHU 7KD RUVD 5KD 72000 T 11155 V C 7KRM 148.7 7KU RUHU 7KD MEVD 7KD 36000 T 12520 V C 9KRR 148.8 9KU RUHU 9KD RUVD 9KD 36000 T 12560 V C 9KRM 148.7 9KU RUHU 9KD MEVD 11KD 36000 T 12600 V C 11KRR 148.8 11KU RUHU 11KD RUVD 13KD 36000 T 12640 V C 11KRM 148.7 11KU RUHU 11KD MEVD 15KD 36000 T 12680 V C 13KRR 148.8 13KU RUHU 13KD RUVD

17KD 36000 T 12720 V C 13KRM 148.7 13KU RUHU 13KD MEVD 19KD 72000 T 11495 V C 15KRR 148.8 15KU RUHU 15KD RUVD 21KD 72000 T 11575 V C 15KRM 148.7 15KU RUHU 15KD MEVD 23KD 72000 T 11655 V C 17KRR 148.8 17KU RUHU 17KD RUVD 2KD 72000 T 10995 H C 17KRM 148.7 17KU RUHU !7KD MEVD 4KD 72000 T 11075 H C 8KEE 157.5 8KU EIVU 8KD EIHD 6KD 72000 T 11155 H C 8KEW 158 8KU EIVU 8KD WIHD 18KD 112000 T 11515 H C 10KEE 157.5 10KU EIVU 10KD EIHD 20KD 112000 T 11635 H C 10KEW 158 10KU EIVU 10KD WIHD 8KD 72000 T 12538 H C 12KEE 157.5 12KU EIVU 12KD EIHD 10KD 36000 T 12600 H C 12KEW 158 12KU EIVU 12KD WIHD 12KD 36000 T 12640 H C 14KEE 157.5 14KU EIVU 14KD EIHD 14KD 36000 T 12680 H C 14KEW 158 14KU EIVU 14KD WIHD 16KD 36000 T 12720 H C 16KEE 157.5 16KU EIVU 16KD EIHD CMD1 1000 R 14002 H T 16KEW 158 16KU EIVU 16KD WIHD CMD2 1000 R 14004.5 H T 8KWE 156.8 8KU WIVU 8KD EIHD CMD3 1000 R 14002 L T 8KWW 157.3 8KU WIVU 8KD WIHD CMD4 1000 R 14004.5 L T 10KWE 156.8 10KU WIVU 10KD EIHD CMD5 1000 R 14002 L T 10KWW 157.3 10KU WIVU 10KD WIHD CMD6 1000 R 14004.5 L T 12KWE 156.8 12KU WIVU 12KD EIHD TLM1 500 T 11698 V T 12KWW 157.3 12KU WIVU 12KD WIHD TLM2 500 T 11699 V T 14KWE 156.8 14KU WIVU 14KD EIHD TLM3 500 T 11698 R T 14KWW 157.3 14KU WIVU 14KD WIHD TLM4 500 T 11699 R T 16KWE 156.8 16KU WIVU 16KD EIHD TLM5 500 T 11698 R T 16KWW 157.3 16KU WIVU 16KD WIHD TLM6 500 T 11699 R T UPC1 25 T 10951 H T UPC2 25 T 10952 V T UPC3 25 T 11451 H T UPC4 25 T 11451.5 V T UPC5 25 T 12748 V T UPC6 25 T 12749 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) D1 36M0G7W 36000 4 27769.6 0.5 3.4 9.5 D2 72M0G7W 72000 4 55539.3 0.5 3.4 13.3 D3 112MG7W 112000 4 86394.3 0.5 3.4 8.7 D4 10M3G7W 10300 4 6240 0.5 3.9 13.8 D5 100KG7W 100 4 70.4 0.5 3 13 D6 1M45G7W 1450 2 614.5 0.5 3.4 15.5 D7 400KG7W 400 2 153.5 0.5 3.4 15.4

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 15.6 1.5 10 20.3

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) 1K 17KMR A1 1 Link-budgets.p 4000 54.6 13.3 21.3 41 47 -145.1 19.1 1K 17KMR D1 1 S13_SCHEDUL 54.6 15 23 42.8 48.8 -152.1 19.1 1K 17KMR D4 3 S13_SCHEDUL 54.6 8.5 16.5 36.3 42.3 -152.1 19.3 1K 17KMR D5 360 S13_SCHEDUL 54.6 -11 -3 16.8 22.8 -152.1 19 1K 17KMR D6 24 S13_SCHEDUL 54.6 1.1 9.1 28.9 34.9 -152.1 19 1K 17KMR D7 90 S13_SCHEDUL 42 -10 -2 22.2 28.2 -152.8 31.6 1K 17KMR A1 2 36000 S13_SCHEDUL 4000 54.6 10.6 18.6 39 47 -145.1 19.7 1K 17KMR D2 1 S13_SCHEDUL 54.6 15.3 23.3 43.8 51.8 -152.1 19.7 1K 17KMR D4 6 S13_SCHEDUL 54.6 5.8 13.8 34.3 42.3 -152.1 20 1K 17KMR D5 720 S13_SCHEDUL 54.6 -13.7 -5.7 14.8 22.8 -152.1 19.6 1K 17KMR D6 49 S13_SCHEDUL 54.6 -1.6 6.4 26.9 34.9 -152.1 19.6 1K 17KMR D7 180 S13_SCHEDUL 43.3 -11.2 -3.2 20 28 -153 30.9 1K 17KMR A1 3 S13_SCHEDUL 4000 54.7 11 21 39 47 -145.1 19.9 1K 17KMR D3 1 S13_SCHEDUL 54.7 13.7 23.7 45.7 53.7 -152.1 19.8 1K 17KMR D4 10 S13_SCHEDUL 54.7 6.2 16.2 34.3 42.3 -152.1 20 1K 17KMR D5 1120 S13_SCHEDUL 54.7 -13.3 -3.3 14.8 22.8 -152.1 19.6 1K 17KMR D6 77 S13_SCHEDUL 54.7 -1.2 8.8 26.9 34.9 -152.1 19.6 1K 17KMR D7 280 S13_SCHEDUL 43.4 -12.4 -2.4 20.3 28.3 -152.7 30.9 1K 17KMR A1 1 S13_SCHEDUL 4000 54.6 15 21 41 47 -145.1 19.1 1K 17KMR D1 1 S13_SCHEDUL 54.6 17.8 23.8 42.8 48.8 -152.1 19.1 1K 17KMR D4 3 S13_SCHEDUL 54.6 12.3 18.3 36.3 42.3 -152.1 19.3 1K 17KMR D5 360 S13_SCHEDUL 54.6 -7.2 -1.2 16.8 22.8 -152.1 19 1K 17KMR D6 24 S13_SCHEDUL 54.6 4.9 10.9 28.9 34.9 -152.1 19 1K 17KMR D7 90 S13_SCHEDUL 42 -7.9 -1.9 22.5 28.5 -152.5 31.6 1K 17KMR A1 1 S13_SCHEDUL 4000 54.6 14.3 20.3 39 47 -145.1 20 1K 17KMR D1 1 S13_SCHEDUL 54.6 16.1 22.1 40.8 48.8 -152.1 20.2 1K 17KMR D5 3 S13_SCHEDUL 54.6 9.6 15.6 34.3 42.3 -152.1 20.8 1K 17KMR D6 360 S13_SCHEDUL 54.6 -9.9 -3.9 14.8 22.8 -152.1 19.9 1K 17KMR D6 24 S13_SCHEDUL 54.6 2.2 8.2 26.9 34.9 -152.1 19.8

1K 17KMR D7 90 S13_SCHEDUL 42.8 -8.6 -2.6 20.3 28.3 -152.7 31.6 1K 17KMR A1 2 S13_SCHEDUL 4000 54.6 14 20 37.1 43.1 -149 25.8 1K 17KMR D2 1 S13_SCHEDUL 54.6 17.9 23.9 40.9 46.9 -157 26.8 1K 17KMR D4 6 S13_SCHEDUL 54.6 9.9 15.9 32.9 38.9 -155.5 25.8 1K 17KMR D5 720 S13_SCHEDUL 54.6 -10.7 -4.7 12.3 18.3 -156.6 26 1K 17KMR D6 49 S13_SCHEDUL 54.6 1 7 24 30 -157 26.4 1K 17KMR D7 180 S13_SCHEDUL 49.5 -9.6 -3.6 18.3 24.3 -156.7 31.5 1K 17KMR A1 2 S13_SCHEDUL 4000 54.6 14 20 40.5 46.5 -145.6 19.4 1K 17KMR D2 1 S13_SCHEDUL 54.6 17.9 23.9 44.3 50.3 -153.6 19.9 1K 17KMR D4 6 S13_SCHEDUL 54.6 9.9 15.9 36.3 42.3 -152.1 19.4 1K 17KMR D5 720 S13_SCHEDUL 54.6 -10.7 -4.7 15.7 21.7 -153.2 19.5 1K 17KMR D6 49 S13_SCHEDUL 54.6 -7.5 -1.5 27 33 -154 23.7 1K 17KMR D7 180 S13_SCHEDUL 46.6 -6.9 -0.9 21.5 27.5 -153.5 31.6 1K 17KMR A1 2 S13_SCHEDUL 4000 54.6 13.9 19.9 40.5 46.5 -145.6 19.4 1K 17KMR D2 1 S13_SCHEDUL 54.6 17.7 23.7 44.3 50.3 -153.6 19.9 1K 17KMR D4 6 S13_SCHEDUL 54.6 9.7 15.7 36.3 42.3 -152.1 19.4 1K 17KMR D5 720 S13_SCHEDUL 54.6 -10.8 -4.8 15.7 21.7 -153.2 19.5 1K 17KMR D6 49 S13_SCHEDUL 54.6 0.8 6.8 27.4 33.4 -153.6 19.7 1K 17KMR D7 179 S13_SCHEDUL 42.6 -6.8 -0.8 21.8 27.8 -153.2 31.6 1K 17KMR A1 2 S13_SCHEDUL 4000 54.6 13.9 19.9 37.1 43.1 -149 25.8 1K 17KMR D2 1 S13_SCHEDUL 54.6 17.7 23.7 40.9 46.9 -157 26.8 1K 17KMR D4 6 S13_SCHEDUL 54.6 9.7 15.7 32.9 38.9 -155.5 25.8 1K 17KMR D5 720 S13_SCHEDUL 54.6 -10.8 -4.8 12.3 18.3 -156.6 26 1K 17KMR D6 49 S13_SCHEDUL 54.6 0.8 6.8 24 30 -157 26.4 1K 17KMR D7 180 S13_SCHEDUL 49.4 -13.1 -7.1 17.9 23.9 -157.1 31.5

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: 3400 INTERNATIONAL DRIVE 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 1227 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1287 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2514 22.3 0.856 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 534 5.1 0.83 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 29.7 7.4 0.71 S16. SPACECRAFT ELECTRICAL CHARACTERISTICS: 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: 2009-04-13 11:45:09
Document Modified: 2009-04-13 11:45:09
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