Attachment Schedule S Tech Data

This document pretains to SAT-LOI-20081113-00216 for Letter of Intent on a Satellite Space Stations filing.

IBFS_SATLOI2008111300216_680414

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: BSSNET119W 12/30/2012 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 6/30/2009 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 10/30/2011 222 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: 12/30/2011 12/30/2011 5328 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) 17.3 G 17.7 G T Broadcasting Satellite Service - Data 17.3 G 17.7 G T Broadcasting Satellite Service - Sound 17.3 G 17.7 G T Broadcasting Satellite Service - Video 17.3 G 17.7 G T TTC 24.75 G 25.25 G R Broadcasting Satellite Service - Data 24.75 G 25.25 G R Broadcasting Satellite Service - Sound 24.75 G 25.25 G R Broadcasting Satellite Service - Video 24.75 G 25.25 G R TTC 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: 118.8 W Available Appendix F offset orbital location 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) CONUS+ S USA, HWA, ALS NESPOT S USA, North of 38N, East of 100WL SESPOT S USA, South of 38N, East of 100WL WSPOT S USA, West of 100 WL HISPOT S HWA LAUL S ULLA SA.gxt Sample spot LA Uplink CMD S ULLA SA.gxt Command station located in LA ULSPOT S Example of 7 Feeder Links TEL S ULLA SA.gxt Telemetry station located in LA CRBSPOT S ABW, ATN ALSSPOT S ALS

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) USA T 36.4 21.4 0.15 30 N CONUS+ 1.8 298 61.1 SP28 T 47.7 45 0.1 30 N NESPOT 2.5 11.5 58.3 SP48 T 47.7 45 0.1 30 N SESPOT 2.5 22 61.1 SP31 T 47.7 45 0.1 30 N WSPOT 2.5 5.3 54.9 SP50 T 47.7 45 0.1 30 N HISPOT 2.5 5.5 55.1 LAUL R 47 46 0.1 30 N LAUL 794 17.5 -109 25 0.5 CMD R 47 46 0.1 30 N LAUL 794 17.5 SP01 T 47.7 45 0.1 30 N WSPOT 2.5 5.6 55.2 SP02 T 47.7 45 0.1 30 N WSPOT 2.5 5.7 55.3 SP03 T 47.7 45 0.1 30 N WSPOT 2.5 5.6 55.2 SP04 T 47.7 45 0.1 30 N WSPOT 2.5 5.6 55.2 SP05 T 47.7 45 0.1 30 N WSPOT 2.5 5.7 55.3 SP06 T 47.7 45 0.1 30 N WSPOT 2.5 5.7 55.3 SP07 T 47.7 45 0.1 30 N NESPOT 2.5 11.5 58.3 SP08 T 47.7 45 0.1 30 N NESPOT 2.5 11.7 58.4 SP09 T 47.7 45 0.1 30 N WSPOT 2.5 5.5 55.1 SP10 T 47.7 45 0.1 30 N WSPOT 2.5 5.5 55.1 SP11 T 47.7 45 0.1 30 N WSPOT 2.5 5.5 55.1 SP12 T 47.7 45 0.1 30 N WSPOT 2.5 5.5 55.1 SP13 T 47.7 45 0.1 30 N WSPOT 2.5 5.5 55.1 SP14 T 47.7 45 0.1 30 N WSPOT 2.5 5.6 55.2 SP15 T 47.7 45 0.1 30 N NESPOT 2.5 11.3 58.2 SP16 T 47.7 45 0.1 30 N NESPOT 2.5 11.5 58.3 SP17 T 47.7 45 0.1 30 N NESPOT 2.5 11.7 58.4 SP18 T 47.7 45 0.1 30 N NESPOT 2.5 12 58.5 SP19 T 47.7 45 0.1 30 N WSPOT 2.5 5.4 55 SP20 T 47.7 45 0.1 30 N WSPOT 2.5 5.4 55 SP21 T 47.7 45 0.1 30 N WSPOT 2.5 5.4 55 SP22 T 47.7 45 0.1 30 N WSPOT 2.5 5.4 55

SP23 T 47.7 45 0.1 30 N WSPOT 2.5 5.4 55 SP24 T 47.7 45 0.1 30 N WSPOT 2.5 5.5 55.1 SP25 T 47.7 45 0.1 30 N NESPOT 2.5 11 58.1 SP26 T 47.7 45 0.1 30 N NESPOT 2.5 11.1 58.2 SP27 T 47.7 45 0.1 30 N NESPOT 2.5 11.3 58.2 SP29 T 47.7 45 0.1 30 N NESPOT 2.5 11.8 58.4 SP30 T 47.7 45 0.1 30 N WSPOT 2.5 5.3 54.9 SP32 T 47.7 45 0.1 30 N WSPOT 2.5 5.3 54.9 SP33 T 47.7 45 0.1 30 N WSPOT 2.5 5.3 54.9 SP34 T 47.7 45 0.1 30 N WSPOT 2.5 5.3 55 SP35 T 47.7 45 0.1 30 N WSPOT 2.5 5.4 55 SP36 T 47.7 45 0.1 30 N SESPOT 2.5 21.6 61.1 SP37 T 47.7 45 0.1 30 N SESPOT 2.5 21.9 61.1 SP38 T 47.7 45 0.1 30 N SESPOT 2.5 22.2 61.2 SP39 T 47.7 45 0.1 30 N NESPOT 2.5 11.4 58.3 SP40 T 47.7 45 0.1 30 N WSPOT 2.5 5.2 54.9 SP41 T 47.7 45 0.1 30 N WSPOT 2.5 5.2 54.9 SP42 T 47.7 45 0.1 30 N WSPOT 2.5 5.3 54.9 SP43 T 47.7 45 0.1 30 N WSPOT 2.5 5.3 55 SP44 T 47.7 45 0.1 30 N SESPOT 2.5 21.4 61 SP45 T 47.7 45 0.1 30 N SESPOT 2.5 21.7 61.1 SP46 T 47.7 45 0.1 30 N SESPOT 2.5 22 61 SP47 T 47.7 45 0.1 30 N SESPOT 2.5 21 60.9 SP49 T 47.7 45 0.1 30 N ALSSPOT 2.5 6.2 55.6 SP51 T 47.7 45 0.1 30 N CRBSPOT 2.5 22.7 61.3 SP52 T 47.7 45 0.1 30 N CRBSPOT 2.5 23.4 61.4 SP53 T 47.7 45 0.1 30 N ALSSPOT 2.5 6 55.4 ES1 R 47 46 0.1 30 N ULSPOT 794 17.5 -109 25 0.5 ES2 R 47 46 0.1 30 N ULSPOT 794 17.5 -109 25 0.5 ES3 R 47 46 0.1 30 N ULSPOT 794 17.5 -109 25 0.5 ES4 R 47 46 0.1 30 N ULSPOT 794 17.5 -109 25 0.5 ES5 R 47 46 0.1 30 N ULSPOT 794 17.5 -109 25 0.5 ES6 R 47 46 0.1 30 N ULSPOT 794 17.5 -109 25 0.5 ES7 R 47 46 0.1 30 N ULSPOT 794 17.5 -109 25 0.5 TEL T 36.4 29 0.15 30 N TEL 2 0.05 23.4 CMD R 47.7 46 0.1 30 N CRBSPOT 794 18.7 TELC T 47.7 46 0.1 30 N CRBSPOT 2 0.1 37.7

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) USA T C -118.8 119 Conus.gxt -116.4 -116.3 -116.2 -116 -115.9 SP50 T C -118.8 SP50.gxt -122.4 -122.3 -122.2 -122.1 -122 SP02 T C -118.8 SP02.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP01 T C -118.8 SP01.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP04 T C -118.8 SP04.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP05 T C -118.8 SP05.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP06 T C -118.8 SP06.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP07 T C -118.8 SP07.gxt -119.2 -119.1 -119 -118.8 -118.7 SP08 T C -118.8 SP08.gxt -119.2 -119.1 -119 -118.8 -118.7 SP09 T C -118.8 SP09.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP10 T C -118.8 SP10.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP11 T C -118.8 SP11.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP12 T C -118.8 SP12.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP13 T C -118.8 SP13.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP14 T C -118.8 SP14.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP15 T C -118.8 SP15.gxt -119.2 -119.1 -119 -118.8 -118.7 SP16 T C -118.8 SP16.gxt -119.2 -119.1 -119 -118.8 -118.7 SP28 T C -118.8 SP28.gxt -119.2 -119.1 -119 -118.8 -118.7 SP31 T C -118.8 SP31.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP48 T C -118.8 SP48.gxt -116.4 -116.3 -116.2 -116 -115.9 LAUL R C -118.8 ULLA G.gxt SP03 T C -118.8 SP03.gxt -122.6 -122.5 -122.4 -122.2 -122.1 CMD R C -118.8 ULLA G.gxt SP17 T C -118.8 SP17.gxt -119.2 -119.1 -119 -118.8 -118.7 SP18 T C -118.8 SP18.gxt -119.2 -119.1 -119 -118.8 -118.7 SP19 T C -118.8 SP19.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP20 T C -118.8 SP20.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP21 T C -118.8 SP21.gxt -122.6 -122.5 -122.4 -122.2 -122.1

SP22 T C -118.8 SP22.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP23 T C -118.8 SP23.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP24 T C -118.8 SP24.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP25 T C -118.8 SP25.gxt -119.2 -119.1 -119 -118.8 -118.7 SP26 T C -118.8 SP26.gxt -119.2 -119.1 -119 -118.8 -118.7 SP27 T C -118.8 SP27.gxt -119.2 -119.1 -119 -118.8 -118.7 SP29 T C -118.8 SP29.gxt -119.2 -119.1 -119 -118.8 -118.7 SP30 T C -118.8 SP30.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP32 T C -118.8 SP32.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP33 T C -118.8 SP33.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP34 T C -118.8 SP34.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP35 T C -118.8 SP35.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP36 T C -118.8 SP36.gxt -116.4 -116.3 -116.2 -116 -115.9 SP37 T C -118.8 SP37.gxt -116.4 -116.3 -116.2 -116 -115.9 SP38 T C -118.8 SP38.gxt -116.4 -116.3 -116.2 -116 -115.9 SP39 T C -118.8 SP39.gxt -119.2 -119.1 -119 -118.8 -118.7 SP40 T C -118.8 SP40.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP41 T C -118.8 SP41.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP42 T C -118.8 SP42.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP43 T C -118.8 SP43.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP44 T C -118.8 SP44.gxt -116.4 -116.3 -116.2 -116 -115.9 SP45 T C -118.8 SP45.gxt -116.4 -116.3 -116.2 -116 -115.9 SP46 T C -118.8 SP46.gxt -116.4 -116.3 -116.2 -116 -115.9 SP47 T C -118.8 SP47.gxt -116.4 -116.3 -116.2 -116 -115.9 SP49 T C -118.8 SP49.gxt -122.6 -122.5 -122.4 -122.2 -122.1 SP51 T C -118.8 SP51.gxt -116.4 -116.3 -116.2 -116 -115.9 SP52 T C -118.8 SP52.gxt -116.4 -116.3 -116.2 -116 -115.9 SP53 T C -118.8 SP53.gxt -122.6 -122.5 -122.4 -122.2 -122.1 TEL T C -118.8 119 Conus.gxt -140.5 -140.5 -140.5 -140.5 -140.5 CMD R C -118.8 SP51R.gxt TELC T C -118.8 SP51.gxt -126.2 -126.2 -126.2 -126.2 -126.2

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) FA001 26000 T 17325 L C NA001 156 GA001 LAUL FA001 USA FA003 26000 T 17354.16 L C NA002 156 GA003 LAUL FA003 USA FA005 26000 T 17383.32 L C NA003 156 GA005 LAUL FA005 USA FA007 26000 T 17412.48 L C NA004 156 GA007 LAUL FA007 USA FA009 26000 T 17441.64 L C NA005 156 GA009 LAUL FA009 USA FA011 26000 T 17470.8 L C NB001 156 GB002 LAUL FB002 USA FA013 26000 T 17499.96 L C NB002 156 GB004 LAUL FB004 USA FA015 26000 T 17529.12 L C NB003 156 GB006 LAUL FB006 USA FA017 26000 T 17558.28 L C NB004 156 GB008 LAUL FB008 USA FA019 26000 T 17587.44 L C NB005 156 GB010 LAUL FB010 USA FA021 26000 T 17616.6 L C 00001 156 GB002 ES1 FB012 SP01 FA023 26000 T 17645.76 L C 00002 156 GB004 ES1 FB014 SP01 FA025 26000 T 17674.92 L C 00003 156 GB006 ES1 FB016 SP01 FB002 26000 T 17325 R C 00004 156 GB008 ES1 FB018 SP01 FB004 26000 T 17354.16 R C 00005 156 GB010 ES1 FB020 SP02 FB006 26000 T 17383.32 R C 00006 156 GB012 ES1 FB022 SP02 FB008 26000 T 17412.48 R C 00007 156 GB014 ES1 FB024 SP02 FB010 26000 T 17441.64 R C 00008 156 GB016 ES1 FB026 SP02 FB012 26000 T 17470.8 R C 00009 156 GA017 ES1 FA011 SP09 FB014 26000 T 17499.96 R C 00010 156 GA019 ES1 FA013 SP09 FB016 26000 T 17529.12 R C 00011 156 GA021 ES1 FA015 SP09 FB018 26000 T 17558.28 R C 00012 156 GA023 ES1 FA017 SP09 FB020 26000 T 17587.44 R C 00013 156 GA025 ES1 FA019 SP10 FB022 26000 T 17616.6 R C 00014 156 GA027 ES1 FA021 SP10 FB024 26000 T 17645.76 R C 00015 156 GA029 ES1 FA023 SP10 FB026 26000 T 17674.92 R C 00016 156 GA031 ES1 FA025 SP10 GA001 26000 R 24775 R C 00017 156 GB002 ES1 FB012 SP20 GA003 26000 R 24804.16 R C 00018 156 GB004 ES1 FB014 SP20 GA005 26000 R 24833.32 R C 00019 156 GB006 ES1 FB016 SP20 GA007 26000 R 24862.48 R C 00020 156 GB008 ES1 FB018 SP20

GA009 26000 R 24891.64 R C 00021 156 GB010 ES1 FB020 SP21 GA011 26000 R 24920.8 R C 00022 156 GB012 ES1 FB022 SP21 GA013 26000 R 24949.96 R C 00023 156 GB014 ES1 FB024 SP21 GA015 26000 R 24979.12 R C 00024 156 GB016 ES1 FB026 SP21 GA017 26000 R 25008.28 R C 00025 156 GB018 ES1 FB012 SP31 GA019 26000 R 25037.44 R C 00026 156 GB020 ES1 FB014 SP31 GA021 26000 R 25066.6 R C 00027 156 GB022 ES1 FB016 SP31 GA023 26000 R 25095.76 R C 00028 156 GB024 ES1 FB018 SP31 GA025 26000 R 25124.92 R C 00029 156 GA025 ES1 FA019 SP32 GA027 26000 R 25154.08 R C 00030 156 GA027 ES1 FA021 SP32 GA029 26000 R 25183.24 R C 00031 156 GA029 ES1 FA023 SP32 GA031 26000 R 25212.4 R C 00032 156 GA031 ES1 FA025 SP32 GB002 26000 R 24775 L C 00033 156 GB002 ES2 FB012 SP03 GB004 26000 R 24804.16 L C 00034 156 GB004 ES2 FB014 SP03 GB006 26000 R 24833.32 L C 00035 156 GB006 ES2 FB016 SP03 GB008 26000 R 24862.48 L C 00036 156 GB008 ES2 FB018 SP03 CMD1 1000 R 24753 R T 00037 156 GB010 ES2 FB020 SP04 TLM1 1000 T 17303 R T 00038 156 GB012 ES2 FB022 SP04 TLM2 1000 T 17306 R T 00039 156 GB014 ES2 FB024 SP04 GB010 26000 R 24891.64 L C 00040 156 GB016 ES2 FB026 SP04 GB012 26000 R 24920.8 L C 00041 156 GA017 ES2 FA011 SP11 GB014 26000 R 24949.96 L C 00042 156 GA019 ES2 FA013 SP11 GB016 26000 R 24979.12 L C 00043 156 GA021 ES2 FA015 SP11 GB018 26000 R 25008.28 L C 00044 156 GA023 ES2 FA017 SP11 GB020 26000 R 25037.44 L C 00045 156 GA025 ES2 FA019 SP12 GB022 26000 R 25066.6 L C 00046 156 GA027 ES2 FA021 SP12 GB024 26000 R 25095.76 L C 00047 156 GA029 ES2 FA023 SP12 GB026 26000 R 25124.92 L C 00048 156 GA031 ES2 FA025 SP12 GB028 26000 R 25154.08 L C 00049 156 GB002 ES2 FB012 SP22 GB030 26000 R 25183.24 L C 00050 156 GB004 ES2 FB014 SP22 GB032 26000 R 25212.4 L C 00051 156 GB006 ES2 FB016 SP22 CMD2 1000 R 24755 R T 00052 156 GB008 ES2 FB018 SP22 00053 156 GB010 ES2 FB020 SP23 00054 156 GB012 ES2 FB022 SP23 00055 156 GB014 ES2 FB024 SP23 00056 156 GB016 ES2 FB026 SP23 00057 156 GB018 ES2 FB012 SP33 00058 156 GB020 ES2 FB014 SP33 00059 156 GB022 ES2 FB016 SP33

00060 156 GB024 ES2 FB018 SP33 00061 156 GA025 ES2 FA019 SP34 00062 156 GA027 ES2 FA021 SP34 00063 156 GA029 ES2 FA023 SP34 00064 156 GA031 ES2 FA025 SP34 00065 156 GB002 ES3 FB012 SP05 00066 156 GB004 ES3 FB014 SP05 00067 156 GB006 ES3 FB016 SP05 00068 156 GB008 ES3 FB018 SP05 00069 156 GB010 ES3 FB020 SP06 00070 156 GB012 ES3 FB022 SP06 00071 156 GB014 ES3 FB024 SP06 00072 156 GB016 ES3 FB026 SP06 00073 156 GA017 ES3 FA011 SP13 00074 156 GA019 ES3 FA013 SP13 00075 156 GA021 ES3 FA015 SP13 00076 156 GA023 ES3 FA017 SP13 00077 156 GA025 ES3 FA019 SP14 00078 156 GA027 ES3 FA021 SP14 00079 156 GA029 ES3 FA023 SP14 00080 156 GA031 ES3 FA025 SP14 00081 156 GB002 ES3 FB012 SP24 00082 156 GB004 ES3 FB014 SP24 00083 156 GB006 ES3 FB016 SP24 00084 156 GB008 ES3 FB018 SP24 00085 156 GB010 ES3 FB020 SP25 00086 156 GB012 ES3 FB022 SP25 00087 156 GB014 ES3 FB024 SP25 00088 156 GB016 ES3 FB026 SP25 00089 156 GB018 ES3 FB012 SP35 00090 156 GB020 ES3 FB014 SP35 00091 156 GB022 ES3 FB016 SP35 00092 156 GB024 ES3 FB018 SP35 00093 156 GA025 ES3 FA019 SP36 00094 156 GA027 ES3 FA021 SP36 00095 156 GA029 ES3 FA023 SP36 00096 156 GA031 ES3 FA025 SP36 00097 156 GB002 ES4 FB012 SP07 00098 156 GB004 ES4 FB014 SP07

00099 156 GB006 ES4 FB016 SP07 00100 156 GB008 ES4 FB018 SP07 00101 156 GB010 ES4 FB020 SP08 00102 156 GB012 ES4 FB022 SP08 00103 156 GB014 ES4 FB024 SP08 00104 156 GB016 ES4 FB026 SP08 00105 156 GA017 ES4 FA011 SP15 00106 156 GA019 ES4 FA013 SP15 00107 156 GA021 ES4 FA015 SP15 00108 156 GA023 ES4 FA017 SP15 00109 156 GA025 ES4 FA019 SP16 00110 156 GA027 ES4 FA021 SP16 00111 156 GA029 ES4 FA023 SP16 00112 156 GA031 ES4 FA025 SP16 00113 156 GB002 ES4 FB012 SP26 00114 156 GB004 ES4 FB014 SP26 00115 156 GB006 ES4 FB016 SP26 00116 156 GB008 ES4 FB018 SP26 00117 156 GB010 ES4 FB020 SP27 00118 156 GB012 ES4 FB022 SP27 00119 156 GB014 ES4 FB024 SP27 00120 156 GB016 ES4 FB026 SP27 00121 156 GB018 ES4 FB012 SP37 00122 156 GB020 ES4 FB014 SP37 00123 156 GB022 ES4 FB016 SP37 00124 156 GB024 ES4 FB018 SP37 00125 156 GA025 ES4 FA019 SP38 00126 156 GA027 ES4 FA021 SP38 00127 156 GA029 ES4 FA023 SP38 00128 156 GA031 ES4 FA025 SP38 00129 156 GB002 ES5 FB012 SP28 00130 156 GB004 ES5 FB014 SP28 00131 156 GB006 ES5 FB016 SP28 00132 156 GB008 ES5 FB018 SP28 00133 156 GB010 ES5 FB020 SP29 00134 156 GB012 ES5 FB022 SP29 00135 156 GB014 ES5 FB024 SP29 00136 156 GB016 ES5 FB026 SP29 00137 156 GA017 ES5 FA011 SP39

00138 156 GA019 ES5 FA013 SP39 00139 156 GA021 ES5 FA015 SP39 00140 156 GA023 ES5 FA017 SP39 00141 156 GA025 ES5 FA019 SP47 00142 156 GA027 ES5 FA021 SP47 00143 156 GA029 ES5 FA023 SP47 00144 156 GA031 ES5 FA025 SP47 00145 156 GB002 ES5 FB012 SP45 00146 156 GB004 ES5 FB014 SP45 00147 156 GB006 ES5 FB016 SP45 00148 156 GB008 ES5 FB018 SP45 00149 156 GB010 ES5 FB020 SP46 00150 156 GB012 ES5 FB022 SP46 00151 156 GB014 ES5 FB024 SP46 00152 156 GB016 ES5 FB026 SP46 00153 156 GB018 ES5 FB012 SP17 00154 156 GB020 ES5 FB014 SP17 00155 156 GB022 ES5 FB016 SP17 00156 156 GB024 ES5 FB018 SP17 00157 156 GA025 ES5 FA019 SP18 00158 156 GA027 ES5 FA021 SP18 00159 156 GA029 ES5 FA023 SP18 00160 156 GA031 ES5 FA025 SP18 00161 156 GB002 ES6 FB012 SP43 00162 156 GB004 ES6 FB014 SP43 00163 156 GB006 ES6 FB016 SP43 00164 156 GB008 ES6 FB018 SP43 00165 156 GB010 ES6 FB020 SP44 00166 156 GB012 ES6 FB022 SP44 00167 156 GB014 ES6 FB024 SP44 00168 156 GB016 ES6 FB026 SP44 00169 156 GA017 ES6 FA011 SP48 00170 156 GA019 ES6 FA013 SP48 00171 156 GA021 ES6 FA015 SP48 00172 156 GA023 ES6 FA017 SP48 00173 156 GA025 ES6 FA019 SP30 00174 156 GA027 ES6 FA021 SP30 00175 156 GA029 ES6 FA023 SP30 00176 156 GA031 ES6 FA025 SP30

00177 156 GB002 ES6 FB012 SP51 00178 156 GB004 ES6 FB014 SP51 00179 156 GB006 ES6 FB016 SP51 00180 156 GB008 ES6 FB018 SP51 00181 156 GB010 ES6 FB020 SP42 00182 156 GB012 ES6 FB022 SP42 00183 156 GB014 ES6 FB024 SP42 00184 156 GB016 ES6 FB026 SP42 00185 156 GB018 ES6 FB012 SP53 00186 156 GB020 ES6 FB014 SP53 00187 156 GB022 ES6 FB016 SP53 00188 156 GB024 ES6 FB018 SP53 00189 156 GB002 ES7 FB012 SP41 00190 156 GB004 ES7 FB014 SP41 00191 156 GB006 ES7 FB016 SP41 00192 156 GB008 ES7 FB018 SP41 00193 156 GB010 ES7 FB020 SP40 00194 156 GB012 ES7 FB022 SP40 00195 156 GB014 ES7 FB024 SP40 00196 156 GB016 ES7 FB026 SP40 00197 156 GB010 ES7 FB020 SP19 00198 156 GB012 ES7 FB022 SP19 00199 156 GB014 ES7 FB024 SP19 00200 156 GB016 ES7 FB026 SP19 00201 156 GA025 ES7 FA019 SP50 00202 156 GA027 ES7 FA021 SP50 00203 156 GA029 ES7 FA023 SP50 00204 156 GA031 ES7 FA025 SP50 00205 156 GB010 ES7 FB020 SP52 00206 156 GB012 ES7 FB022 SP52 00207 156 GB014 ES7 FB024 SP52 00208 156 GB016 ES7 FB026 SP52 00209 156 GA025 ES7 FA019 SP49 00210 156 GA027 ES7 FA021 SP49 00211 156 GA029 ES7 FA023 SP49 00212 156 GA031 ES7 FA025 SP49 C1 CMD1 CMD C2 CMD2 CMD T1 TLM1 TEL

T2 TLM2 TEL C1CRB CMD1 CMDCR C2CRB CMD2 CMDCR T1CRB TLM1 TELCR T2CRB TLM2 TELCR

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 25M8G7W 25800 8 42570 0.67 7.1 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) C1 800KF9D 800 40 50 T1 800KF9D 800 10 30

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) NA001 NB005 D1 1 Comm link CO 67.6 7 14.9 46.1 61.1 -115 16.4 00001 00212 D1 1 Comm link Spo 67.6 8 30.4 59.1 61.1 -115 16.4 C1 C2 C1 Command Link 64.4 5.5 24.5 17.5 T1 T2 T1 Telemetry Link 16 23.4 -140.5 41.2 C1CRB C2CRB C1 64.4 5.5 24.5 18.7 T1CRB T2CRB T1 37.7 37.7 -126.2 41.2

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: S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Curacao S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):

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 3715 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2684 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6339 50 0.6 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 277 8.2 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 80 7.3 0.51 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): 14822 14822 14822 14822 Bus (Watts): (b): (g): (l): (q): 1766 955 1766 955 Total (Watts): (c): (h): (m): (r): 16688 15877 16688 15877 Solar Array (Watts): (d): (i): (n): (s): 20892 18568 19792 17602 Depth of Battery (e) (j) (o) (t) Discharge (%): 75 % 75 % 75 % 75 % 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? X YES NO 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: 2008-11-25 10:48:40
Document Modified: 2008-11-25 10:48:40
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