Attachment Sched S Tech Report

This document pretains to SAT-MOD-20130322-00052 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2013032200052_999945

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 10 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 48 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: 1728 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) 5925 M 6425 M R Fixed Satellite Service 3700 M 4200 M T Fixed Satellite Service 14000 M 14500 M R Fixed Satellite Service 11450 M 11700 M T Fixed Satellite Service 12250 M 12500 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: 47.5 E Replace the Intelsat 709 spacecraft and to provide Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be service to Africa, Asia, and Europe. 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 of (l) Argument of Active Service Arc Range (Degrees) Plane No. Satellites in Angle (degrees) Period the Ascending Node Perigee (m) Begin (n) End Angle (o) Other Plane (Seconds) (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) 1 S Global 2 S Asia 3 S Europe and Africa 4 S Europe and Middle East 5 S Europe and Asia

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) GHC T 26.4 20.4 90 1 41.4 GVC T 26.8 20.8 01 41.8 AVK T 32.2 26.2 02 49 EHK T 29.5 23.5 90 3 47.4 EVK T 30.2 24.2 03 47.6 EMK T 32.6 26.6 04 49.3 ESK T 32.1 26.1 90 5 49.1 INKD T 35.1 29.1 90 2 52 TGK T 23 20.6 90 1 6.4 TPKD T -1.1 -3.5 1 2.1 UVK T 18.4 16 01 11.3 UHK T 18.4 16 90 1 11.2 GHC R 28.2 22.2 90 1 0.4 -104.4 25 1 GVC R 27.7 21.7 01 -0.4 -103.6 25 1 AVK R 32.9 26.9 02 4.4 -99.4 25 1 EHK R 30.4 24.4 90 3 2.1 -97.1 25 1 EVK R 29.8 23.8 03 2.3 -97.3 25 1 EMK R 33.6 27.6 04 4.8 -99.8 25 1 ESK R 34.7 28.7 90 5 6.4 -101.4 25 1 TGK R 23.7 21.3 90 1 -11.8 -105.1 TPKU R -1.2 -3.6 90 1 -32.8 -84.4 TBKD T -5.3 -6.4 1 1.4 TBKU R -0.5 -1.6 90 1 -31.9 -85

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 Gain Max. Power Flux Density (dBW/M2/Hz) Beam T/R Cross Ref. Orbital Contour Description Contour Data (GXT File) At Angle of Arrival above horizontal (for emission with highest PFD) ID Mode Polar Longitude (Figure/Table/ Exhibit) (g) 5 Deg (h) 10 Deg (i) 15 Deg (j) 20 Deg (k) 25 Deg Mode ("C" (Deg. E/W) or" X") GHC T C 47.5 ghcd.gxt -158.8 -158.7 -158.6 -158.5 -158.4 GVC T C 47.5 gvcd.gxt -158.4 -158.3 -158.2 -158.1 -158 AVK T C 47.5 avkd.gxt -152.5 -152.4 -152.3 -152.1 -152 EHK T C 47.5 ehkd.gxt -154.1 -154 -153.9 -153.7 -153.6 EVK T C 47.5 evkd.gxt -153.9 -153.8 -153.7 -153.5 -153.4 EMK T C 47.5 emkd.gxt -152.2 -152.1 -152 -151.8 -151.7 ESK T C 47.5 eskd.gxt -152.4 -152.3 -152.2 -152 -151.9 INKD T C 47.5 inkd.gxt -149.5 -149.4 -149.3 -149.1 -149 TGK T C 47.5 TGKD.gxt -171.6 -171.5 -171.4 -171.3 -171.2 TPKD T C 47.5 tpkd.gxt -175.9 -175.8 -175.7 -175.6 -175.5 UVK T C 47.5 uvkd.gxt -159.9 -159.8 -159.7 -159.6 -159.5 UHK T C 47.5 uhkd.gxt -160 -159.9 -159.8 -159.7 -159.6 GHC R C 47.5 ghcu.gxt GVC R C 47.5 gvcu.gxt AVK R C 47.5 avku.gxt EHK R C 47.5 ehku.gxt EVK R C 47.5 evku.gxt EMK R C 47.5 emku.gxt ESK R C 47.5 esku.gxt TGK R C 47.5 TGKU.gxt TPKU R C 47.5 tpku.gxt TBKD T C 47.5 tbkd.gxt -176.6 -176.5 -176.4 -176.3 -176.2 TBKU R C 47.5 tbku.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) ES5KD 36000 T 11637 H C MF16K 121.4 M16KU EMKU F16KD EHKD ES6KD 36000 T 11677 H C MF17K 121.4 M17KU EMKU F17KD EHKD ES1KU 36000 R 14020 H C MF18K 121.4 M18KU EMKU F18KD EHKD ES2KU 36000 R 14060 H C MI13K 120.4 M13KU EMKU I13KD INKD ES3KU 36000 R 14100 H C MI14K 120.4 M14KU EMKU I14KD INKD ES4KU 36000 R 14140 H C MA21K 120.3 M15KU EMKU A21KD AVKD ES5KU 36000 R 14180 H C MA22K 120.3 M16KU EMKU A22KD AVKD ES6KU 36000 R 14220 H C MA23K 120.3 M17KU EMKU A23KD AVKD M7KU 36000 R 14020 V C MA24K 120.3 M18KU EMKU A24KD AVKD M8KU 36000 R 14060 V C EF13K 122.7 F13KU EVKU F13KD EHKD M9KU 36000 R 14100 V C EF14K 122.7 F14KU EVKU F14KD EHKD M10KU 36000 R 14140 V C EF15K 122.7 F15KU EVKU F15KD EHKD M11KU 36000 R 14180 V C EF16K 122.7 F16KU EVKU F16KD EHKD M12KU 36000 R 14220 V C EF17K 122.7 F17KU EVKU F17KD EHKD M7KD 36000 T 11477 V C EF18K 122.7 F18KU EVKU F18KD EHKD M8KD 36000 T 11517 V C EF19K 121.4 F19KU EHKU F19KD EVKD M9KD 36000 T 11557 V C EF20K 121.4 F20KU EHKU F20KD EVKD M10KD 36000 T 11597 V C EF21K 121.4 F21KU EHKU F21KD EVKD M11KD 36000 T 11637 V C EF22K 121.4 F22KU EHKU F22KD EVKD M12KD 36000 T 11677 V C EF23K 121.4 F23KU EHKU F23KD EVKD I28KD 36000 T 12392 H C EF24K 121.4 F24KU EHKU F24KD EVKD I29KD 36000 T 12432 H C FI13K 121.7 F13KU EVKU I13KD INKD I30KD 36000 T 12472 H C FI14K 121.7 F14KU EVKU I14KD INKD M13KU 36000 R 14270 V C FA21K 121.6 F15KU EVKU A21KD AVKD M14KU 36000 R 14310 V C FA22K 121.6 F16KU EVKU A22KD AVKD M15KU 36000 R 14350 V C FA23K 121.6 F17KU EVKU A23KD AVKD M16KU 36000 R 14390 V C FA24K 121.6 F18KU EVKU A24KD AVKD M17KU 36000 R 14430 V C AS1K 120.8 A7KU AVKU ES1KD ESKD F13KD 36000 T 12522 H C AS2K 120.8 A8KU AVKU ES2KD ESKD F14KD 36000 T 12562 H C AS3K 120.8 A9KU AVKU ES3KD ESKD

F15KD 36000 T 12602 H C AI25K 120.7 A7KU AVKU I25KD INKD F16KD 36000 T 12642 H C AI26K 120.7 A8KU AVKU I26KD INKD F17KD 36000 T 12682 H C AI27K 120.7 A9KU AVKU I27KD INKD F18KD 36000 T 12722 H C AM10K 120.5 A10KU AVKU M10KD EMKD M18KU 36000 R 14470 V C AM11K 120.5 A11KU AVKU M11KD EMKD I14KD 36000 T 12562 H C AM12K 120.5 A12KU AVKU M12KD EMKD A21KD 36000 T 12602 V C AI13K 120.7 A13KU AVKU I13KD INKD A22KD 36000 T 12642 V C AI14K 120.7 A14KU AVKU I14KD INKD A23KD 36000 T 12682 V C A21K 120.6 A15KU AVKU A21KD AVKD A24KD 36000 T 12722 V C A22K 120.6 A16KU AVKU A22KD AVKD I13KD 36000 T 12522 H C A23K 120.6 A17KU AVKU A23KD AVKD F13KU 36000 R 14270 V C A24K 120.6 A18KU AVKU A24KD AVKD F14KU 36000 R 14310 V C AF15K 121.7 A15KU AVKU F15KD EHKD F15KU 36000 R 14350 V C AF16K 121.7 A16KU AVKU F16KD EHKD F16KU 36000 R 14390 V C AF17K 121.7 A17KU AVKU F17KD EHKD F17KU 36000 R 14430 V C AF18K 121.7 A18KU AVKU F18KD EHKD F18KU 36000 R 14470 V C G1C 128.5 G1CU GHCU G1CD GHCD F19KU 36000 R 14270 H C G2C 128.5 G2CU GHCU G2CD GHCD F20KU 36000 R 14310 H C G3C 128.5 G3CU GHCU G3CD GHCD F21KU 36000 R 14350 H C G4C 128.5 G4CU GHCU G4CD GHCD F22KU 36000 R 14390 H C G5C 128.5 G5CU GHCU G5CD GHCD G1CU 54000 R 5955 H C G6C 128.5 G6CU GHCU G6CD GHCD G2CU 54000 R 6015 H C G7C 128.5 G7CU GHCU G7CD GHCD G3CU 54000 R 6075 H C G8C 128.5 G8CU GHCU G8CD GHCD G4CU 54000 R 6143 H C G9C 128.5 G9CU GHCU G9CD GHCD G5CU 27000 R 6199 H C G10C 128.5 G10CU GHCU G10CD GHCD G6CU 27000 R 6229 H C G11C 128.5 G11CU GHCU G11CD GHCD G7CU 27000 R 6259 H C G12C 128.5 G12CU GHCU G12CD GHCD G8CU 27000 R 6289 H C G13C 128.2 G13CU GVCU G13CD GVCD G9CU 27000 R 6319 H C G14C 128.2 G14CU GVCU G14CD GVCD G10CU 27000 R 6349 H C G15C 128.2 G15CU GVCU G15CD GVCD G11CU 27000 R 6379 H C G16C 128.2 G16CU GVCU G16CD GVCD G12CU 27000 R 6409 H C G17C 128.2 G17CU GVCU G17CD GVCD G13CU 54000 R 5955 V C G18C 128.2 G18CU GVCU G18CD GVCD G14CU 54000 R 6015 V C G19C 128.2 G19CU GVCU G19CD GVCD G15CU 54000 R 6075 V C G20C 128.2 G20CU GVCU G20CD GVCD G16CU 54000 R 6143 V C G21C 128.2 G21CU GVCU G21CD GVCD G17CU 27000 R 6199 V C G22C 128.2 G22CU GVCU G22CD GVCD G18CU 27000 R 6229 V C G23C 128.2 G23CU GVCU G23CD GVCD

G19CU 27000 R 6259 V C G24C 128.2 G24CU GVCU G24CD GVCD G20CU 27000 R 6289 V C ES1K 121 ES1KU ESKU ES1KD ESKD G21CU 27000 R 6319 V C ES2K 121 ES2KU ESKU ES2KD ESKD G22CU 27000 R 6349 V C ES3K 121 ES3KU ESKU ES3KD ESKD G23CU 27000 R 6379 V C ES4K 121 ES4KU ESKU ES4KD ESKD G24CU 27000 R 6409 V C ES5K 121 ES5KU ESKU ES5KD ESKD G1CD 54000 T 3730 H C ES6K 121 ES6KU ESKU ES6KD ESKD G2CD 54000 T 3790 H C EM7K 120.2 M7KU EMKU M7KD EMKD G3CD 54000 T 3850 H C EM8K 120.2 M8KU EMKU M8KD EMKD G4CD 54000 T 3918 H C EM9K 120.2 M9KU EMKU M9KD EMKD G5CD 27000 T 3974 H C EM10K 120.2 M10KU EMKU M10KD EMKD G6CD 27000 T 4004 H C EM11K 120.2 M11KU EMKU M11KD EMKD G7CD 27000 T 4034 H C EM12K 120.2 M12KU EMKU M12KD EMKD G8CD 27000 T 4064 H C MI28K 120.4 M10KU EMKU I28KD INKD G9CD 27000 T 4094 H C MI29K 120.4 M11KU EMKU I29KD INKD G10CD 27000 T 4124 H C MI30K 120.4 M12KU EMKU I30KD INKD G11CD 27000 T 4154 H C MF13K 121.4 M13KU EMKU F13KD EHKD G12CD 27000 T 4184 H C MF14K 121.4 M14KU EMKU F14KD EHKD G13CD 54000 T 3730 V C MF15K 121.4 M15KU EMKU F15KD EHKD G14CD 54000 T 3790 V C G15CD 54000 T 3850 V C G16CD 54000 T 3918 V C G17CD 27000 T 3974 V C G18CD 27000 T 4004 V C G19CD 27000 T 4034 V C G20CD 27000 T 4064 V C G21CD 27000 T 4094 V C G22CD 27000 T 4124 V C G23CD 27000 T 4154 V C G24CD 27000 T 4184 V C ES1KD 36000 T 11477 H C ES2KD 36000 T 11517 H C ES3KD 36000 T 11557 H C ES4KD 36000 T 11597 H C F23KU 36000 R 14430 H C F24KU 36000 R 14470 H C F19KD 36000 T 12522 V C F20KD 36000 T 12562 V C F21KD 36000 T 12602 V C

F22KD 36000 T 12642 V C F23KD 36000 T 12682 V C F24KD 36000 T 12722 V C A7KU 36000 R 14020 V C A8KU 36000 R 14060 V C A9KU 36000 R 14100 V C A10KU 36000 R 14140 V C A11KU 36000 R 14180 V C A12KU 36000 R 14220 V C I25KD 36000 T 12272 H C I26KD 36000 T 12312 H C I27KD 36000 T 12352 H C A13KU 36000 R 14270 V C A14KU 36000 R 14310 V C A15KU 36000 R 14350 V C A16KU 36000 R 14390 V C A17KU 36000 R 14430 V C A18KU 36000 R 14470 V C CMD 1000 R 14499.5 H T CMDP 1000 R 14000.5 R T CMDB 1000 R 14499.5 H T TM1 120 T 12747.5 H T TM2 120 T 12748.5 H T TM1P 120 T 12747.5 R T TM2P 120 T 12748.5 R T TM1B 120 T 12747.5 H T TM2B 120 T 12748.5 H T ULPC1 25 T 11699 V T ULPC2 25 T 11699 V T ULPC3 25 T 12749.5 H T ULPC4 25 T 12749.5 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 54MG07W 39997 4 36860 0.5 3.36 8.4 D2 36M0G7W 30133 4 24575 0.5 3.36 16 D4 1M45G7W 1229 2 512 0.5 3.4 14.8 D5 400KG7W 302 4 256 0.5 3.4 15.6 D6 200KG7W 154 2 64 0.5 3.4 15.5 D3 3M07G7W 2413 4 2048 0.5 2.99 15.7

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 36M0F3W 36000 TV/FM 1 PAL 15.6 1.5 10 22.2

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) G1C AF18K D4 24 1450 IS-10 Ku-Band 46.4 3.1 9.1 23.4 29.4 -157.6 33.1 G1C AF18K D6 180 200 IS-10 Ku-Band 46.4 -5 1 15.3 21.3 -156.7 31 G1C AF18K D3 17 3075 IS-10 C-Band Li 43.2 12.5 18.5 19.6 25.6 -164.3 28.4 G1C AF18K D3 11 3075 IS-10 Ku-Band 46.4 7.2 13.2 27.5 33.5 -156.4 31 G1C AF18K D2 1 36000 IS-10 Ku-Band 52.7 12.8 18.8 41.4 47.4 -153.5 26.7 G1C AF18K D5 135 400 IS-10 C-Band Li 43.2 3.5 9.5 10.6 16.6 -164.3 28.4 G1C AF18K D5 90 400 IS-10 Ku-Band 46.4 -1.9 4.1 18.4 24.4 -156.5 31 G1C AF18K D1 1 54000 IS-10 C-Band Li 58.4 9.1 15.1 35.4 41.4 -160.7 28.4 G1C AF18K A1 1 36000 IS-10 C-Band Li 4000 58.4 16.1 22.1 35.4 41.4 -150.7 33 G1C AF18K A1 1 36000 IS-10 Ku-Band 4000 52.7 19.8 25.8 41.4 47.4 -144.7 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): 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: 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: 2013-06-12 09:49:14
Document Modified: 2013-06-12 09:49:14
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