Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20050523-00106 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2005052300106_434331

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: SKYTERRA-1 4/19/2010 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 4/19/2008 12 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 84 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: 9485.5 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) 18.3 G 18.8 G T Fixed Satellite Service 19.7 G 20.2 G T Fixed Satellite Service 28.35 G 28.6 G R Fixed Satellite Service 29.25 G 30 G R Fixed Satellite Service 5926.25 M 5926.75 M R Fixed Satellite Service 6424.25 M 6424.75 M R Fixed Satellite Service 3700.75 M 3701.25 M T Fixed Satellite Service 4198.75 M 4199.25 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: 95 W Spectrum availability and look angle performance Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be across service area. 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 Continental United States

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) SPU1 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU2 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU3 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU4 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU5 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU6 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU7 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU8 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU9 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU1 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU1 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU1 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU1 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU1 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU1 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU1 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU1 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU1 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU1 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU2 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 SPU2 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 RU1 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU2 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU3 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU4 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU5 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU6 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU7 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU8 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1

RU9 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU10 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU11 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU12 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU13 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU14 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU15 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU16 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 RU17 R 43.1 39.1 0.11 0.01 30 N CONUS 832 13.9 -69.5 15 1 SPD1 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 22.49 65.72 SPD2 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 22.49 65.72 SPD3 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 36.55 67.83 SPD4 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 36.55 67.83 SPD5 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 36.55 67.83 SPD6 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 44.99 68.73 SPD7 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 14.06 63.68 SPD8 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 39.36 68.15 SPD9 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 22.49 65.72 SPD1 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 36.55 67.83 SPD1 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 36.55 67.83 SPD1 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 44.99 68.73 SPD1 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 22.49 65.72 SPD1 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 22.49 65.72 SPD1 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD1 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD1 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD1 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD1 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD2 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 36.55 67.83 SPD2 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 36.55 67.83 RD1 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD2 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD3 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD4 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD5 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD6 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD7 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD8 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD9 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8

RD10 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD11 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD12 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD13 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD14 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD15 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD16 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 RD17 T 43.1 39.1 0.11 0.01 30 N CONUS 2.1 37 58.8 CON T 36 26 0.11 0.01 30 N CONUS 2.5 292.4 60.66 CON T 36 26 0.11 0.01 30 N CONUS 2.5 292.4 60.66 OMN T 0 -4 0.11 0.01 30 N 0 CONUS 3.6 16.2 12.1 TLML T 28 25 0.11 0.01 30 N CONUS 2.8 0.166 20.2 OMN R 0 -4 0.11 0.01 30 N 0 CONUS 1000 -30 OMN T 0 -4 0.11 0.01 30 N 90 CONUS 3.6 16.2 12.1 OMN R 0 -4 0.11 0.01 30 N 90 CONUS 1000 -30

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) CON T C -95 CONL.gxt -118 -118 -118 -118 -118 CON T C -95 CONR.gxt -118 -118 -118 -118 -118 TLML T C -95 TLML.gxt -134.4 -134.4 -134.4 -134.4 -134.4

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) U1 85000 R 29872.5 R C SR1 90.9 U1 SPU1 D1 SPD1 D1 85000 T 18522.5 L C SR2 90.9 U1 SPU2 D1 SPD2 U2 10500 R 29795 L C SR3 93 U1 SPU3 D1 SPD3 D2 10500 T 18445 L C SR4 93 U1 SPU4 D1 SPD4 U3 10500 R 29774 L C SR5 93 U1 SPU5 D1 SPD5 D3 10500 T 18424 L C SR6 93.9 U1 SPU6 D1 SPD6 U4 10500 R 29754 L C SR7 88.9 U1 SPU7 D1 SPD7 D4 10500 T 18404 L C SR8 93.3 U1 SPU8 D1 SPD8 U5 10500 R 29733 L C SR9 90.9 U1 SPU9 D1 SPD9 D5 10500 T 18383 L C SR10 93 U1 SPU10 D1 SPD10 U6 60000 R 29655 R C SR11 93 U1 SPU11 D1 SPD11 D6A 60000 T 18770 L C SR12 93.9 U1 SPU12 D1 SPD12 D6B 60000 T 18716 R C SR13 90.9 U1 SPU13 D1 SPD13 D6C 60000 T 18662 L C SR14 90.9 U1 SPU14 D1 SPD14 D6D 60000 T 18608 R C SR15 94.9 U1 SPU15 D1 SPD15 U7 292000 R 29406 R C SR16 94.9 U1 SPU16 D1 SPD16 D7 292000 T 19851 L C SR17 94.9 U1 SPU17 D1 SPD17 U8 46250 R 28398.125 R C SR18 94.9 U1 SPU18 D1 SPD18 U9 46250 R 28444.375 R C SR19 94.9 U1 SPU19 D1 SPD19 U10 46250 R 28490.625 R C SR20 93 U1 SPU20 D1 SPD20 U11 46250 R 28536.875 R C SR21 93 U1 SPU21 D1 SPD21 D8A 46250 T 20028.125 L C RR1 90.9 U2 RU1 D2 SPD1 D9A 46250 T 20074.375 R C RR2 90.9 U3 RU2 D3 SPD2 D10A 46250 T 20120.625 L C RR3 93 U2 RU3 D2 SPD3 D11A 46250 T 20166.875 R C RR4 93 U3 RU4 D3 SPD4 D8B 46250 T 20028.125 R C RR5 93 U2 RU5 D2 SPD5 D9B 46250 T 20074.375 L C RR6 93.9 U3 RU6 D3 SPD6 D10B 46250 T 20120.625 R C RR7 88.9 U4 RU7 D4 SPD7 D11B 46250 T 20166.875 L C RR8 93.3 U5 RU8 D5 SPD8 C1 500 R 5926.5 H T RR9 90.9 U4 RU9 D4 SPD9

C2 500 R 6424.5 V T RR10 93 U5 RU10 D5 SPD10 C3 500 R 29999.5 R T RR11 93 U4 RU11 D4 SPD11 T1 500 T 3701 H T RR12 93.9 U5 RU12 D5 SPD12 T2 500 T 4199 V T RR13 90.9 U3 RU13 D3 SPD13 T3 500 T 20198 L T RR14 90.9 U2 RU14 D2 SPD14 RR15 94.9 U3 RU15 D3 SPD15 RR16 94.9 U2 RU16 D2 SPD16 RR17 94.9 U3 RU17 D3 SPD17 RF1 111.7 U6 SPU1 D6A RD1 RF2 111.7 U6 SPU2 D6B RD2 RF3 111.7 U6 SPU3 D6A RD3 RF4 111.7 U6 SPU4 D6B RD4 RF5 111.7 U6 SPU5 D6A RD5 RF6 111.7 U6 SPU6 D6B RD6 RF7 111.7 U6 SPU7 D6C RD7 RF8 111.7 U6 SPU8 D6D RD8 RF9 111.7 U6 SPU9 D6C RD9 RF10 111.7 U6 SPU10 D6D RD10 RF11 111.7 U6 SPU11 D6C RD11 RF12 111.7 U6 SPU12 D6D RD12 RF13 111.7 U6 SPU13 D6B RD13 RF14 111.7 U6 SPU14 D6A RD14 RF15 111.7 U6 SPU15 D6B RD15 RF16 111.7 U6 SPU16 D6A RD16 RF17 111.7 U6 SPU17 D6B RD17 SF1 90.7 U7 SPU1 D7 SPD1 SF2 90.7 U7 SPU2 D7 SPD2 SF3 92.8 U7 SPU3 D7 SPD3 SF4 92.8 U7 SPU4 D7 SPD4 SF5 92.8 U7 SPU5 D7 SPD5 SF6 93.7 U7 SPU6 D7 SPD6 SF7 88.7 U7 SPU7 D7 SPD7 SF8 93.1 U7 SPU8 D7 SPD8 SF9 90.7 U7 SPU9 D7 SPD9 SF10 92.8 U7 SPU10 D7 SPD10 SF11 92.8 U7 SPU11 D7 SPD11 SF12 93.7 U7 SPU12 D7 SPD12 SF13 90.7 U7 SPU13 D7 SPD13 SF14 90.7 U7 SPU14 D7 SPD14

SF15 94.7 U7 SPU15 D7 SPD15 SF16 94.7 U7 SPU16 D7 SPD16 SF17 94.7 U7 SPU17 D7 SPD17 SF18 94.7 U7 SPU18 D7 SPD18 SF19 94.7 U7 SPU19 D7 SPD19 SF20 92.8 U7 SPU20 D7 SPD20 SF21 92.8 U7 SPU21 D7 SPD21 CF1 121.8 U8 SPU7 D8A CONL CF2 121.8 U9 SPU8 D9A CONR CF3 121.8 U10 SPU9 D10A CONL CF4 121.8 U11 SPU10 D11A CONR CF5 121.8 U8 SPU13 D8B CONR CF6 121.8 U9 SPU14 D9B CONL CF7 121.8 U10 SPU15 D10B CONR CF8 121.8 U11 SPU21 D11B CONL C1 C1 OMNRH C2 C2 OMNRV C3 C3 SPU17 T1 T1 OMNTH T2 T2 OMNTV T3 T3 TLML

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 2M70G7W 2700 4 2149 0.691 5.1 17.3 D2 248KG7W 248 4 197 0.691 5.1 17.3 D3 60M0G7W 60000 4 47748 0.691 5.1 17.3 D4 36M5G7W 36500 4 29022 0.691 5.1 17.3 D5 46M3G7W 46250 4 36805 0.691 5.1 17.3

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 500KF1D 500 1 10 22.2 A2 500KG1D 500 1 9 21.2 A3 500KF1D 500 1 10 22.2 A4 500KG1D 500 1 10.4 22.6

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) SR1 SR21 D1 31 2741.935 SR LB.doc 44.3 1 5 28.8 38.8 -127.6 37.7 RR1 RR17 D2 42 256 RR LB.doc 44.3 -6.5 -2.5 19.6 29.6 -126.5 37.7 RF1 RF17 D3 1 RF LB.doc 62.9 4.4 8.4 54.8 58.8 -121 19.1 SF1 SF21 D4 8 36500 SF LB.doc 62.9 2 6 49.6 59.6 -118 19.5 CF1 CF8 D5 1 CF LB.doc 62.9 2 6 50.7 60.7 -118 19.6 C1 C2 A1 1 C1 LB.doc 53 20.3 25.3 C3 C3 A2 1 Ka CMD LB.do 62.9 -20 -9 T1 T2 A3 1 T1 LB.doc 8.1 12.1 -166 24.5 T3 T3 A4 1 Ka TLM LB.doc 17.2 20.2 -134 37.7

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

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 2769 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3454 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6223 35 0.9 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 880 3 0.89 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 82.5 3.6 0.8 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): 12563 12563 12563 12563 Bus (Watts): (b): (g): (l): (q): 2651 1409 2651 1409 Total (Watts): (c): (h): (m): (r): 15214 13972 15214 13972 Solar Array (Watts): (d): (i): (n): (s): 19200 16205 17112 14681 Depth of Battery (e) (j) (o) (t) Discharge (%): 76.8 % 76.8 % 76.8 % 76.8 % 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: 2005-05-27 12:51:10
Document Modified: 2005-05-27 12:51:10
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