Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20041029-00205 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2004102900205_403523

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 & 2 Y b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 12 Years 64 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 64 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: MHz GSO NGSO 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 29.25 G 30 G R Fixed Satellite Service 28.35 G 28.6 G R 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 Degrees E/W 0.05 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) SVC1 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 Flux Density (Y/N) Value Size (dB) (dBW) Temp (k) Pt. (dBW/m2) CU R 54.9 53.9 0.05 35 N SVC1 936 26.2 -80 30 1 CD T 37 33 0.05 35 N SVC1 2.5 297 55.73 SFU R 55.2 54.2 0.05 35 N SVC1 936 22.81 -80 30 1 SFD T 52.3 48.5 0.05 35 N SVC1 2.5 10.67 58.82 SRU R 50.8 46.3 0.05 35 N SVC1 936 22.81 -80 30 1 SRD T 61.4 60.4 0.05 35 N SVC1 2.5 0.072 35.27 RFU R 55.3 54.3 0.05 35 N SVC1 936 29.56 -80 30 1 RFD T 43.6 39.5 0.05 35 N SVC1 2.5 25.91 61.78 RRU R 41.9 37.9 0.05 35 N SVC1 936 13.85 -80 30 1 RRD T 61.4 60.4 0.05 35 N SVC1 2.5 0.102 35.31 TM T 6 0 1 35 N SVC1 1 20 19

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) CF R C -95 CU R X -95 conus.cov.itu CD T X -95 conus.tx.itu -118 -118 -118 -118 -118 SFU R X -95 CF R C -95 CU R X -95 conus.cov.itu CD T X -95 conus.tx.itu -118 -118 -118 -118 -118 SFU R X -95 CF R C -95 CU R X -95 conus.cov.itu CD T X -95 conus.tx.itu -118 -118 -118 -118 -118 SFU R X -95

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) (c) (d) Center (e) (f) TTC (a) (b) Receive Band Transmit Band Channel Assigned T/R Frequency Polarization or Comm Transponder Transponder (c) Channel (d) Beam (e) Channel (f) Beam ID No. Bandwidth Mode (MHz) (H, V, L, R) Channel ID Gain (dB) No. ID No. (kHz) (T or C) CH1U 9920 R 29772.70 R C C1 200 CH26U CU CH26D CD CH1D 9920 T 18422.71 L C C2 200 CH58U CU CH58D CD CH2U 9920 R 29783.20 R C SPF1 200 CH50U SFU CH50D SFD CH2D 9920 T 18433.21 L C SPF2 200 CH18U SFU CH18D SFD CH3U 9920 R 29793.70 R C SPF3 200 CH19U SFU CH19D SFD CH3D 9920 T 18443.71 L C SPF4 200 CH51U SFU CH51D SFD CH4U 9920 R 29804.20 R C SPF5 200 CH20U SFU CH20D SFD CH4D 9920 T 18454.21 L C SPF6 200 CH21U SFU CH21D SFD CH5U 9920 R 29772.70 L C SPF7 200 CH52U SFU CH52D SFD CH5D 9920 T 18422.71 R C SPF8 200 CH53U SFU CH53D SFD CH6U 9920 R 29783.20 L C SPF9 200 CH54U SFU CH54D SFD CH6D 9920 T 18433.21 R C SPF10 200 CH22U SFU CH22D SFD CH7U 9920 R 29793.70 L C SPF11 200 CH23U SFU CH23D SFD CH7D 9920 T 18443.71 R C SPF12 200 CH55U SFU CH55D SFD CH8U 9920 R 29804.20 L C SPF13 200 CH24U SFU CH24D SFD CH8D 9920 T 18454.21 R C SPF14 200 CH25U SFU CH25D SFD CH9U 82800 R 29871.40 L C SPF15 200 CH56U SFU CH56D SFD CH9D 82800 T 18521.40 R C SPF16 200 CH18U SFU CH18D SFD CH10U 58600 R 29665.00 R C SPF17 200 CH57U SFU CH57D SFD CH10D 58600 T 18607.00 L C SPF18 200 CH19U SFU CH19D SFD CH11U 58600 R 29665.00 R C SPF19 200 CH20U SFU CH20D SFD CH11D 58600 T 18661.00 L C SPF20 200 CH50U SFU CH50D SFD CH12U 58600 R 29665.00 R C SPF21 200 CH21U SFU CH21D SFD CH12D 58600 T 18715.00 L C SPF22 200 CH22U SFU CH22D SFD CH13U 58600 R 29665.00 R C SPF23 200 CH23U SFU CH23D SFD CH13D 58600 T 18769.00 L C SPF24 200 CH51U SFU CH51D SFD CH14U 58600 R 29665.00 L C SPF25 200 CH24U SFU CH24D SFD CH14D 58600 T 18607.00 R C SPF26 200 CH52U SFU CH52D SFD CH15U 58600 R 29665.00 L C SPF27 200 CH25U SFU CH25D SFD CH15D 58600 T 18661.00 R C SPF28 200 CH53U SFU CH53D SFD

CH16U 58600 R 29665.00 L C SPF29 200 CH54U SFU CH54D SFD CH16D 58600 T 18715.00 R C SPF30 200 CH55U SFU CH55D SFD CH17U 58600 R 29665.00 L C SPF31 200 CH18U SFU CH18D SFD CH17D 58600 T 18769.00 R C SPF32 200 CH56U SFU CH56D SFD CH18U 36000 R 29279.50 L C SPF33 200 CH57U SFU CH57D SFD CH18D 36000 T 19729.53 R C SPF34 200 CH19U SFU CH19D SFD CH19U 36000 R 29315.50 L C SPF35 200 CH20U SFU CH20D SFD CH19D 36000 T 19765.53 R C SPF36 200 CH21U SFU CH21D SFD CH20U 36000 R 29351.50 L C SPF37 200 CH50U SFU CH50D SFD CH20D 36000 T 19801.53 R C SPF38 200 CH51U SFU CH51D SFD CH21U 36000 R 29387.50 L C SPF39 200 CH52U SFU CH52D SFD CH21D 36000 T 19837.53 R C SPF40 200 CH53U SFU CH53D SFD CH22U 36000 R 29423.50 L C SPF41 200 CH22U SFU CH22D SFD CH22D 36000 T 19873.53 R C SPF42 200 CH54U SFU CH54D SFD CH23U 36000 R 29459.50 L C RGF1 200 CH14U RFU CH14D RFD CH23D 36000 T 19909.53 R C RGF2 200 CH47U RFU CH47D RFD CH24U 36000 R 29495.50 L C RGF3 200 CH10U RFU CH10D RFD CH24D 36000 T 19945.53 R C RGF4 200 CH43U RFU CH43D RFD CH25U 36000 R 29531.50 L C RGF5 200 CH13U RFU CH14D RFD CH25D 36000 T 19981.53 R C RGF6 200 CH47U RFU CH47D RFD CH26U 54000 R 28399.40 R C RGF7 200 CH10U RFU CH10D RFD CH26D 54000 T 20026.42 L C RGF8 200 CH43U RFU CH43D RFD CH27U 54000 R 28444.40 L C RGF9 200 CH14U RFU CH14D RFD CH27D 54000 T 20071.42 R C RGF10 200 CH16U RFU CH16D RFD CH28U 54000 R 28489.40 R C RGF11 200 CH49U RFU CH49D RFD CH28D 54000 T 20116.42 L C RGF12 200 CH12U RFU CH12D RFD CH29U 54000 R 28534.40 L C RGF13 200 CH45U RFU CH45D RFD CH29D 54000 T 20161.42 L C RGF14 200 CH16U RFU CH16D RFD CH30D 500 T 20197.75 L T RGF15 200 CH49U RFU CH49D RFD CH31U 500 R 29950.00 L T RGF16 200 CH12U RFU CH12D RFD CH32U 500 R 29999.50 R T RGF17 200 CH45U RFU CH45D RFD CH33U 9920 R 29772.70 L C RGF18 200 CH16U RFU CH16D RFD CH33D 9920 T 18422.71 R C RGF19 200 CH42U RFU CH42D RFD CH34U 9920 R 29783.20 L C RGF20 200 CH11U RFU CH11D RFD CH34D 9920 T 18433.21 R C RGF21 200 CH46U RFU CH46D RFD CH35U 9920 R 29793.70 L C RGF22 200 CH15U RFU CH15D RFD CH35D 9920 T 18443.71 R C RGF23 200 CH42U RFU CH42D RFD CH36U 9920 R 29804.20 L C RGF24 200 CH11U RFU CH11D RFD CH36D 9920 T 18454.21 L C RGF25 200 CH46U RFU CH46D RFD

CH37U 9920 R 29772.70 R C RGF26 200 CH15U RFU CH15D RFD CH37D 9920 T 18422.71 L C RGF27 200 CH17U RFU CH17D RFD CH38U 9920 R 29783.20 R C RGF28 200 CH44U RFU CH44D RFD CH38D 9920 T 18433.21 L C RGF29 200 CH13U RFU CH13D RFD CH39U 9920 R 29793.70 R C RGF30 200 CH48U RFU CH48D RFD CH39D 9920 T 18443.71 L C RGF31 200 CH17U RFU CH17D RFD CH40U 9920 R 29804.20 R C RGF32 200 CH43U RFU CH43D RFD CH40D 9920 T 18454.21 L C SPR1 200 CH41U SRU CH41D SRD CH41U 82800 R 29871.40 R C SPR2 200 CH9U SRU CH9D SRD CH41D 82800 T 18521.40 L C SPR3 200 CH9U SRU CH9D SRD CH42U 58600 R 29665.00 L C SPR4 200 CH41U SRU CH41D SRD CH42D 58600 T 18607.00 R C SPR5 200 CH9U SRU CH9D SRD CH43U 58600 R 29665.00 L C SPR6 200 CH9U SRU CH9D SRD CH43D 58600 T 18661.00 R C SPR7 200 CH41U SRU CH41D SRD CH44U 58600 R 29665.00 L C SPR8 200 CH41U SRU CH41D SRD CH44D 58600 T 18715.00 R C SPR9 200 CH41U SRU CH41D SRD CH45U 58600 R 29665.00 L C SPR10 200 CH9U SRU CH9D SRD CH45D 58600 T 18769.00 R C SPR11 200 CH9U SRU CH9D SRD CH46U 58600 R 29665.00 R C SPR12 200 CH41U SRU CH41D SRD CH46D 58600 T 18607.00 L C SPR13 200 CH9U SRU CH9D SRD CH47U 58600 R 29665.00 R C SPR14 200 CH9U SRU CH9D SRD CH47D 58600 T 18661.00 L C SPR15 200 CH41U SRU CH41D SRD CH48U 58600 R 29665.00 R C SPR16 200 CH9U SRU CH9D SRD CH48D 58600 T 18715.00 L C SPR17 200 CH41U SRU CH41D SRD CH49U 58600 R 29665.00 R C SPR18 200 CH9U SRU CH9D SRD CH49D 58600 T 18769.00 L C SPR19 200 CH9U SRU CH9D SRD CH50U 36000 R 29279.5 R C SPR20 200 CH41U SRU CH41D SRD CH50D 36000 T 19729.53 L C SPR21 200 CH9U SRU CH9D SRD CH51U 36000 R 29315.50 R C SPR22 200 CH9U SRU CH9D SRD CH51D 36000 T 19765.53 L C SPR23 200 CH9U SRU CH9D SRD CH52U 36000 R 29351.50 R C SPR24 200 CH41U SRU CH41D SRD CH52D 36000 T 19801.53 L C SPR25 200 CH9U SRU CH9D SRD CH53U 36000 R 29387.50 R C SPR26 200 CH41U SRU CH41D SRD CH53D 36000 T 19837.53 L C SPR27 200 CH9U SRU CH9D SRD CH54U 36000 R 29423.50 R C SPR28 200 CH41U SRU CH41D SRD CH54D 36000 T 19873.53 L C SPR29 200 CH41U SRU CH41D SRD CH55U 36000 R 29459.50 R C SPR30 200 CH41U SRU CH40D SRD CH55D 36000 T 19909.53 L C SPR31 200 CH9U SRU CH9D SRD CH56U 36000 R 29495.50 R C TM1 CH30D TM

CH56D 36000 T 19945.53 L C TM2 CH62D TM CH57U 36000 R 29531.50 L C SPR32 200 CH41U SRU CH41D SRD CH57D 36000 T 19981.53 L C SPR33 200 CH41U SRU CH41D SRD CH58U 54000 R 28399.40 L C SPR34 200 CH9U SRU CH9D SRD CH58D 54000 T 20026.42 R C SPR35 200 CH9U SRU CH9D SRD CH59U 54000 R 28444.40 L C SPR36 200 CH9U SRU CH9D SRD CH59D 54000 T 20071.42 L C SPR37 200 CH41U SRU CH41D SRD CH60U 54000 R 28489.40 L C SPR38 200 CH41U SRU CH41D SRD CH60D 54000 T 20116.42 R C SPR39 200 CH41U SRU CH41D SRD CH61U 54000 R 28534.40 R C SPR40 200 CH41U SRU CH41D SRD CH61D 54000 T 20161.42 L C SPR41 200 CH9U SRU CH9D SRD CH62D 500 T 20197.75 R T SPR42 200 CH41U SRU CH41D SRD CH63U 500 R 29950.00 R T RGR1 200 CH5U RRU CH5D RRD CH64U 500 R 29999.50 L T RGR2 200 CH38U RRU CH38D RRD RGR3 200 CH1U RRU CH1D RRD RGR4 200 CH34U RRU CH34D RRD RGR5 200 CH5U RRU CH5D RRD RGR6 200 CH38U RRU CH38D RRD RGR7 200 CH1U RRU CH1D RRD RGR8 200 CH34U RRU CH34D RRD RGR9 200 CH5U RRU CH5D RRD RGR10 200 CH7U RRU CH7D RRD RGR11 200 CH40U RRU CH40D RRD RGR12 200 CH3U RRU CH3D RRD RGR13 200 CH36U RRU CH36D RRD RGR14 200 CH7U RRU CH7D RRD RGR15 200 CH40U RRU CH40D RRD RGR16 200 CH3U RRU CH3D RRD RGR17 200 CH36U RRU CH36D RRD RGR18 200 CH7U RRU CH7D RRD RGR19 200 CH33U RRU CH33D RRD RGR20 200 CH2U RRU CH2D RRD RGR21 200 CH37U RRU CH37D RRD RGR22 200 CH6U RRU CH6D RRD RGR23 200 CH33U RRU CH33D RRD RGR24 200 CH2U RRU CH2D RRD RGR25 200 CH37U RRU CH37D RRD RGR26 200 CH6U RRU CH6D RRD RGR27 200 CH7U RRU CH8D RRD

RGR28 200 CH35U RRU CH35D RRD RGR29 200 CH4U RRU CH4D RRD RGR30 200 CH39U RRU CH39D RRD RGR31 200 CH8U RRU CH8D RRD RGR32 200 CH34U RRU CH34D RRD

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) DO1 1M84GXW 1840 4 60000 0.75 10 20 DO2 58M6GXW 58600 4 60000 0.75 10 20 DO3 9M92G7W 9920 4 128 0.75 10 20 DO4 291MG7W 291000 4 40000 0.75 10 20 DO5 82M8G7W 82800 4 128 0.75 10 20 DO6 5K00G9D 5 4 56 0.75 10 20 DO7 5K00N0N 5 4 56 0.75 10 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. Bandwidth per Carrier NTSC, Weighting SCPC/FM Preemphasis, Objective Objective Companded Baseband Baseband Modulation ID (kHz) PAL, etc. (dB) Modulation and Noise (dB) (dB) Talker Level Freq. (MHz) Freq. (MHz) Index Index Weighting (dB) (dBm0)

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) C1 C2 DO1 4 45000 64.1 -7.59 -4.75 56.4 59.3 -118 22.6 SPF1 SPF42 DO4 8 36400 64.36 -12.94 7.47 51.12 68.32 -118 16.69 RGF1 RGF32 DO2 1 62.9 -3.1 19.8 49.8 69.23 -118 18.28 SPR1 SPR42 DO5 42 2700 43.2 -12.66 2.81 32.36 39.49 -118 36.48 RGR1 RGR32 DO3 31 10500 43.1 -2.81 6.9 37.76 42.37 -118 37.08 TM1 TM2 DO6 1 6 17 17 23 23 -118 -3

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, NW S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Washington, DC DC 20008 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 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 2 0.89 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 100 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): 14000 14000 14000 14000 Bus (Watts): (b): (g): (l): (q): 1800 925 1800 925 Total (Watts): (c): (h): (m): (r): 15800 14925 15800 14925 Solar Array (Watts): (d): (i): (n): (s): 18200 17400 16300 15500 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?: 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 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? 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: 2004-11-02 13:49:15
Document Modified: 2004-11-02 13:49:15
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