Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20050216-00040 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2005021600040_418686

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-2 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 12 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 121 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: 9632 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 SPU4 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 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 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 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 SPU3 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 SPU3 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 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 SPU4 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 RU2 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU4 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU6 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU8 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU11 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU13 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU15 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU17 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1

RU19 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU21 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU23 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU25 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU28 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU30 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU32 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 SPD1 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 39.36 68.15 SPD4 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 22.49 65.72 SPD7 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 39.36 68.15 SPD8 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 39.36 68.15 SPD9 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD1 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD1 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 14.06 63.68 SPD1 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 39.36 68.15 SPD2 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 36.55 67.83 SPD2 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 36.55 67.83 SPD2 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD2 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 22.49 65.72 SPD2 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 22.49 65.72 SPD3 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD3 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 39.36 68.15 SPD3 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD3 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 39.36 68.15 SPD3 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 39.36 68.15 SPD3 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 39.36 68.15 SPD4 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD4 T 52.2 48.1 0.03 0.01 30 N CONUS 2.5 56.23 69.7 RD11 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD17 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD23 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD32 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD2 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD19 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD15 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD25 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD21 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD6 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD30 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8

RD13 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD28 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD8 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD4 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 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 TLM T 28 25 0.11 0.01 30 N CONUS 2.8 0.166 20.2 OMN T 0 -4 0.11 0.01 30 N CONUS 3.6 16.2 12.1 OMN R 0 -4 0.11 0.01 30 N CONUS 1000 -30 OMN T 0 -4 0.11 0.01 30 N CONUS 3.6 16.2 12.1 OMN R 0 -4 0.11 0.01 30 N 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 TLM T C -95 TLMR.gxt -134.4 -134.4 -134.4 -134.4 -134.4 CON T C -95 CONL.gxt -118 -118 -118 -118 -118 CON T C -95 CONR.gxt -118 -118 -118 -118 -118 TLM T C -95 TLMR.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 L C SR1 93.3 U1 SPU1 D1 SPD1 D1 85000 T 18522.5 R C SR2 90.9 U1 SPU4 D1 SPD4 U2 10500 R 29795 R C SR3 93.3 U1 SPU7 D1 SPD7 D2 10500 T 18445 R C SR4 93.3 U1 SPU8 D1 SPD8 U3 10500 R 29774 R C SR5 94.9 U1 SPU9 D1 SPD9 D3 10500 T 18424 R C SR6 94.9 U1 SPU12 D1 SPD12 U4 10500 R 29754 R C SR7 88.9 U1 SPU15 D1 SPD15 D4 10500 T 18404 R C SR8 93.3 U1 SPU17 D1 SPD17 U5 10500 R 29733 R C SR9 93 U1 SPU20 D1 SPD20 D5 10500 T 18383 R C SR10 93 U1 SPU24 D1 SPD24 U6 60000 R 29655 L C SR11 94.9 U1 SPU26 D1 SPD26 D6 60000 T 18716 L C SR12 90.9 U1 SPU28 D1 SPD28 D7 60000 T 18608 L C SR13 90.9 U1 SPU29 D1 SPD29 U7 292000 R 29406 L C SR14 94.9 U1 SPU30 D1 SPD30 D8 292000 T 19851 R C SR15 93.3 U1 SPU32 D1 SPD32 U8 46250 R 28398.125 L C SR16 94.9 U1 SPU33 D1 SPD33 U9 46250 R 28444.375 L C SR17 93.3 U1 SPU37 D1 SPD37 U10 46250 R 28490.625 L C SR18 93.3 U1 SPU38 D1 SPD38 U11 46250 R 28536.875 L C SR19 93.3 U1 SPU39 D1 SPD39 D9 46250 T 20028.125 L C SR20 94.9 U1 SPU40 D1 SPD40 D10 46250 T 20074.375 R C SR21 94.9 U1 SPU42 D1 SPD42 D11 46250 T 20120.625 L C RR1 90.9 U2 RU11 D2 SPD4 D12 46250 T 20166.875 R C RR2 93.3 U2 RU17 D2 SPD7 C1 500 R 5926.5 V C RR3 93.3 U2 RU23 D2 SPD8 C2 500 R 6424.5 H C RR4 94.9 U2 RU32 D2 SPD9 C3 500 R 29998 L C RR5 94.9 U2 RU2 D2 SPD12 T1 500 T 3701 V C RR6 88.9 U2 RU19 D2 SPD15 T2 500 T 4199 H C RR7 93.3 U2 RU15 D2 SPD17 T3 500 T 20199 R C RR8 93 U2 RU25 D2 SPD24 RR9 90.9 U2 RU21 D2 SPD28

RR10 93.3 U2 RU6 D2 SPD32 RR11 94.9 U2 RU30 D2 SPD33 RR12 93.3 U2 RU13 D2 SPD37 RR13 93.3 U2 RU28 D2 SPD38 RR14 94.9 U2 RU8 D2 SPD40 RR15 94.9 U2 RU4 D2 SPD42 RR16 90.9 U3 RU11 D3 SPD4 RR17 93.3 U3 RU17 D3 SPD7 RR18 93.3 U3 RU23 D3 SPD8 RR19 94.9 U3 RU32 D3 SPD9 RR20 94.9 U3 RU2 D3 SPD12 RR21 88.9 U3 RU19 D3 SPD15 RR22 93.3 U3 RU15 D3 SPD17 RR23 93 U3 RU25 D3 SPD24 RR24 90.9 U3 RU21 D3 SPD28 RR25 93.3 U3 RU6 D3 SPD32 RR26 94.9 U3 RU30 D3 SPD33 RR27 93.3 U3 RU13 D3 SPD37 RR28 93.3 U3 RU28 D3 SPD38 RR29 94.9 U3 RU8 D3 SPD40 RR30 94.9 U3 RU4 D3 SPD42 RR31 90.9 U4 RU11 D4 SPD4 RR32 93.3 U4 RU17 D4 SPD7 RR33 93.3 U4 RU23 D4 SPD8 RR34 94.9 U4 RU32 D4 SPD9 RR35 94.9 U4 RU2 D4 SPD12 RR36 88.9 U4 RU19 D4 SPD15 RR37 93.3 U4 RU15 D4 SPD17 RR38 93 U4 RU25 D4 SPD24 RR39 90.9 U4 RU21 D4 SPD28 RR40 93.3 U4 RU6 D4 SPD32 RR41 94.9 U4 RU30 D4 SPD33 RR42 93.3 U4 RU13 D4 SPD37 RR43 93.3 U4 RU28 D4 SPD38 RR44 94.9 U4 RU8 D4 SPD40 RR45 94.9 U4 RU4 D4 SPD42 RR46 90.9 U5 RU11 D5 SPD4 RR47 93.3 U5 RU17 D5 SPD7 RR48 93.3 U5 RU23 D5 SPD8

RR49 94.9 U5 RU32 D5 SPD9 RR50 94.9 U5 RU2 D5 SPD12 RR51 88.9 U5 RU19 D5 SPD15 RR52 93.3 U5 RU15 D5 SPD17 RR53 93 U5 RU25 D5 SPD24 RR54 90.9 U5 RU21 D5 SPD28 RR55 93.3 U5 RU6 D5 SPD32 RR56 94.9 U5 RU30 D5 SPD33 RR57 93.3 U5 RU13 D5 SPD37 RR58 93.3 U5 RU28 D5 SPD38 RR59 94.9 U5 RU8 D5 SPD40 RR60 94.9 U5 RU4 D5 SPD42 RF1 111.7 U6 SPU4 D6 RD11 RF2 111.7 U6 SPU7 D6 RD17 RF3 111.7 U6 SPU8 D7 RD23 RF4 111.7 U6 SPU9 D7 RD32 RF5 111.7 U6 SPU12 D7 RD2 RF6 111.7 U6 SPU15 D7 RD19 RF7 111.7 U6 SPU17 D6 RD15 RF8 111.7 U6 SPU24 D7 RD25 RF9 111.7 U6 SPU28 D7 RD21 RF10 111.7 U6 SPU32 D7 RD6 RF11 111.7 U6 SPU33 D6 RD30 RF12 111.7 U6 SPU37 D6 RD13 RF13 111.7 U6 SPU38 D6 RD28 RF14 111.7 U6 SPU40 D7 RD8 RF15 111.7 U6 SPU42 D7 RD4 SF1 93.3 U7 SPU1 D8 SPD1 SF2 90.9 U7 SPU4 D8 SPD4 SF3 93.3 U7 SPU7 D8 SPD7 SF4 93.3 U7 SPU8 D8 SPD8 SF5 94.9 U7 SPU9 D8 SPD9 SF6 94.9 U7 SPU12 D8 SPD12 SF7 88.9 U7 SPU15 D8 SPD15 SF8 93.3 U7 SPU17 D8 SPD17 SF9 93 U7 SPU20 D8 SPD20 SF10 93 U7 SPU24 D8 SPD24 SF11 94.9 U7 SPU26 D8 SPD26 SF12 90.9 U7 SPU28 D8 SPD28

SF13 90.9 U7 SPU29 D8 SPD29 SF14 94.9 U7 SPU30 D8 SPD30 SF15 93.3 U7 SPU32 D8 SPD32 SF16 94.9 U7 SPU33 D8 SPD33 SF17 93.3 U7 SPU37 D8 SPD37 SF18 93.3 U7 SPU38 D8 SPD38 SF19 93.3 U7 SPU39 D8 SPD39 SF20 94.9 U7 SPU40 D8 SPD40 SF21 94.9 U7 SPU42 D8 SPD42 CF1 121.8 U8 SPU4 D9 CONL CF2 121.8 U9 SPU20 D10 CONR CF3 121.8 U10 SPU28 D11 CONL CF4 121.8 U11 SPU29 D12 CONR C1 C1 OMNRV C2 C2 OMNRH C3 C3 SPU15 T1 T1 OMNTV T2 T2 OMNTH T3 T3 TLMR

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 10 22.2 A2 500KG1D 500 9 21.2 A3 500KF1D 500 10 22.2 A4 500KG1D 500 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 43.2 1 5 28.8 38.8 -127.6 37.7 RR1 RR60 D2 42 256 RR LB.doc 43.2 -6.5 -2.5 19.6 29.6 -126.5 37.7 RF1 RF15 D3 1 RF LB.doc 62.9 -1.1 8.4 57.8 61.8 -118 19.1 SF1 SF21 D4 8 36500 SF LB.doc 62.9 2 6 49.6 59.6 -118 19.1 CF1 CF4 D5 1 CF LB.doc 62.9 2 6 50.7 60.7 -118 19.1 C1 C2 A1 1 C1 LB.doc 53 20.3 25.3 C3 C3 A3 1 Ka CMD LB.do 62.9 -20 9 T1 T2 A2 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 2494 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3140 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5634 24 0.9 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 800 3 0.89 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 60 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): 8598 8598 8598 8598 Bus (Watts): (b): (g): (l): (q): 2731 1428 2731 1428 Total (Watts): (c): (h): (m): (r): 11329 10026 11329 10026 Solar Array (Watts): (d): (i): (n): (s): 13951 11782 12434 10668 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: 2005-02-18 12:15:44
Document Modified: 2005-02-18 12:15:44
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