Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20050214-00038 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2005021400038_418581

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 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: 131 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: 9836 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) 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 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 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 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 SPU4 R 55.2 51.2 0.03 0.01 30 N CONUS 741 26.5 -81.6 15 1 RU1 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU3 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU5 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU7 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU9 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU10 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU12 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU14 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1

RU16 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU18 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU20 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU22 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU24 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU26 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU27 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU29 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 RU31 R 46.1 42.1 0.11 0.01 30 N CONUS 826 16.9 -81.6 15 1 SPD2 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 14.06 63.68 SPD3 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 44.99 68.73 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 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 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 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 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 22.49 65.72 SPD2 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 22.49 65.72 SPD2 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 36.55 67.83 SPD3 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD3 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 56.23 69.7 SPD3 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 22.49 65.72 SPD4 T 52.2 48.2 0.03 0.01 30 N CONUS 2.5 56.23 69.7 RD1 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD3 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD5 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD7 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD9 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD10 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD12 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD14 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD16 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8

RD18 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD20 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD22 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD24 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD26 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD27 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD29 T 46.1 42.1 0.11 0.01 30 N CONUS 2.1 37 61.8 RD31 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 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 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 88.9 U1 SPU2 D1 SPD2 D1 85000 T 18522.5 L C SR2 93.9 U1 SPU3 D1 SPD3 U2 10500 R 29795 L C SR3 93 U1 SPU5 D1 SPD5 D2 10500 T 18445 L C SR4 93.9 U1 SPU6 D1 SPD6 U3 10500 R 29774 L C SR5 94.9 U1 SPU10 D1 SPD10 D3 10500 T 18424 L C SR6 94.9 U1 SPU11 D1 SPD11 U4 10500 R 29754 L C SR7 93 U1 SPU13 D1 SPD13 D4 10500 T 18404 L C SR8 93 U1 SPU14 D1 SPD14 U5 10500 R 29733 L C SR9 90.9 U1 SPU16 D1 SPD16 D5 10500 T 18383 L C SR10 90.9 U1 SPU18 D1 SPD18 U6 60000 R 29655 R C SR11 94.9 U1 SPU19 D1 SPD19 D6 60000 T 18662 R C SR12 93 U1 SPU21 D1 SPD21 D7 60000 T 18770 R C SR13 90.9 U1 SPU22 D1 SPD22 U7 292000 R 29406 R C SR14 94.9 U1 SPU23 D1 SPD23 D8 292000 T 19851 L C SR15 90.9 U1 SPU25 D1 SPD25 U8 46250 R 28398.125 R C SR16 93 U1 SPU27 D1 SPD27 U9 46250 R 28444.375 R C SR17 94.9 U1 SPU31 D1 SPD31 U10 46250 R 28490.625 R C SR18 94.9 U1 SPU34 D1 SPD34 U11 46250 R 28536.875 R C SR19 90.9 U1 SPU35 D1 SPD35 D9 46250 T 20028.125 R C SR20 90.9 U1 SPU36 D1 SPD36 D10 46250 T 20074.375 L C SR21 94.9 U1 SPU41 D1 SPD41 D11 46250 T 20120.625 R C RR1 88.9 U2 RU10 D2 SPD2 D12 46250 T 20166.875 L C RR2 93.9 U2 RU18 D2 SPD3 C1 500 R 5926.5 H T RR3 93 U2 RU16 D2 SPD5 C2 500 R 6424.5 V T RR4 93.9 U2 RU9 D2 SPD6 C3 500 R 29999.5 R T RR5 94.9 U2 RU29 D2 SPD10 T1 500 T 3701 H T RR6 93 U2 RU5 D2 SPD13 T2 500 T 4199 V T RR7 93 U2 RU7 D2 SPD14 T3 500 T 20198 L T RR8 90.9 U2 RU3 D2 SPD16 RR9 90.9 U2 RU20 D2 SPD18

RR10 94.9 U2 RU31 D2 SPD19 RR11 93 U2 RU14 D2 SPD21 RR12 90.9 U2 RU1 D2 SPD22 RR13 90.9 U2 RU12 D2 SPD25 RR14 93 U2 RU22 D2 SPD27 RR15 94.9 U2 RU26 D2 SPD34 RR16 90.9 U2 RU27 D2 SPD35 RR17 94.9 U2 RU24 D2 SPD41 RR18 88.9 U3 RU10 D3 SPD2 RR19 93.9 U3 RU18 D3 SPD3 RR20 93 U3 RU16 D3 SPD5 RR21 93.9 U3 RU9 D3 SPD6 RR22 94.9 U3 RU29 D3 SPD10 RR23 93 U3 RU5 D3 SPD13 RR24 93 U3 RU7 D3 SPD14 RR25 90.9 U3 RU3 D3 SPD16 RR26 90.9 U3 RU20 D3 SPD18 RR27 94.9 U3 RU31 D3 SPD19 RR28 93 U3 RU14 D3 SPD21 RR29 90.9 U3 RU1 D3 SPD22 RR30 90.9 U3 RU12 D3 SPD25 RR31 93 U3 RU22 D3 SPD27 RR32 94.9 U3 RU26 D3 SPD34 RR33 90.9 U3 RU27 D3 SPD35 RR34 94.9 U3 RU24 D3 SPD41 RR35 88.9 U4 RU10 D4 SPD2 RR36 93.9 U4 RU18 D4 SPD3 RR37 93 U4 RU16 D4 SPD5 RR38 93.9 U4 RU9 D4 SPD6 RR39 94.9 U4 RU29 D4 SPD10 RR40 93 U4 RU5 D4 SPD13 RR41 93 U4 RU7 D4 SPD14 RR42 90.9 U4 RU3 D4 SPD16 RR43 90.9 U4 RU20 D4 SPD18 RR44 94.9 U4 RU31 D4 SPD19 RR45 93 U4 RU14 D4 SPD21 RR46 90.9 U4 RU1 D4 SPD22 RR47 90.9 U4 RU12 D4 SPD25 RR48 93 U4 RU22 D4 SPD27

RR49 94.9 U4 RU26 D4 SPD34 RR50 90.9 U4 RU27 D4 SPD35 RR51 94.9 U4 RU24 D4 SPD41 RR52 88.9 U5 RU10 D5 SPD2 RR53 93.9 U5 RU18 D5 SPD3 RR54 93 U5 RU16 D5 SPD5 RR55 93.9 U5 RU9 D5 SPD6 RR56 94.9 U5 RU29 D5 SPD10 RR57 93 U5 RU5 D5 SPD13 RR58 93 U5 RU7 D5 SPD14 RR59 90.9 U5 RU3 D5 SPD16 RR60 90.9 U5 RU20 D5 SPD18 RR61 94.9 U5 RU31 D5 SPD19 RR62 93 U5 RU14 D5 SPD21 RR63 90.9 U5 RU1 D5 SPD22 RR64 90.9 U5 RU12 D5 SPD25 RR65 93 U5 RU22 D5 SPD27 RR66 94.9 U5 RU26 D5 SPD34 RR67 90.9 U5 RU27 D5 SPD35 RR68 94.9 U5 RU24 D5 SPD41 RF1 111.7 U6 SPU2 D6 RD10 RF2 111.7 U6 SPU3 D6 RD18 RF3 111.7 U6 SPU5 D6 RD16 RF4 111.7 U6 SPU6 D7 RD9 RF5 111.7 U6 SPU10 D6 RD29 RF6 111.7 U6 SPU13 D7 RD5 RF7 111.7 U6 SPU14 D7 RD7 RF8 111.7 U6 SPU16 D7 RD3 RF9 111.7 U6 SPU18 D7 RD20 RF10 111.7 U6 SPU19 D6 RD31 RF11 111.7 U6 SPU21 D6 RD14 RF12 111.7 U6 SPU22 D7 RD1 RF13 111.7 U6 SPU25 D6 RD12 RF14 111.7 U6 SPU27 D7 RD22 RF15 111.7 U6 SPU34 D7 RD26 RF16 111.7 U6 SPU35 D6 RD27 RF17 111.7 U6 SPU41 D7 RD24 SF1 88.9 U7 SPU2 D8 SPD2 SF2 93.9 U7 SPU3 D8 SPD3

SF3 93 U7 SPU5 D8 SPD5 SF4 93.9 U7 SPU6 D8 SPD6 SF5 94.9 U7 SPU10 D8 SPD10 SF6 94.9 U7 SPU11 D8 SPD11 SF7 93 U7 SPU13 D8 SPD13 SF8 93 U7 SPU14 D8 SPD14 SF9 90.9 U7 SPU16 D8 SPD16 SF10 90.9 U7 SPU18 D8 SPD18 SF11 94.9 U7 SPU19 D8 SPD19 SF12 93 U7 SPU21 D8 SPD21 SF13 90.9 U7 SPU22 D8 SPD22 SF14 94.9 U7 SPU23 D8 SPD23 SF15 90.9 U7 SPU25 D8 SPD25 SF16 93 U7 SPU27 D8 SPD27 SF17 94.9 U7 SPU31 D8 SPD31 SF18 94.9 U7 SPU34 D8 SPD34 SF19 90.9 U7 SPU35 D8 SPD35 SF20 90.9 U7 SPU36 D8 SPD36 SF21 94.9 U7 SPU41 D8 SPD41 CF1 121.8 U8 SPU2 D9 CONR CF2 121.8 U9 SPU16 D10 CONL CF3 121.8 U10 SPU18 D11 CONR CF4 121.8 U11 SPU35 D12 CONL C1 C1 OMNRH C2 C2 OMNRV C3 C3 SPU2 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 43.2 1 5 28.8 38.8 -127.6 37.7 RR1 RR68 D2 42 256 RR LB.doc 43.2 -6.5 -2.5 19.6 29.6 -126.5 37.7 RF1 RF17 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 2499 (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: 5639 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): 8403 8403 8403 8403 Bus (Watts): (b): (g): (l): (q): 2651 1409 2651 1409 Total (Watts): (c): (h): (m): (r): 11054 9812 11054 9812 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 07:50:58
Document Modified: 2005-02-18 07:50:58
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC