Attachment Schedule S Tech Data

This document pretains to SAT-AMD-20070209-00033 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2007020900033_551828

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: GESN NGSO N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 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: 18000 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) 29.5 G 30.0 G R 4 x 125 MHz channels (only for 3 HEO satellites ) 28.6 G 29.1 G R 4 x 125 MHz channels 47.2 G 47.5 G R Gateway beams 47.5 G 47.9 G R Gateway and user beams 47.9 G 48.2 G R Gateway beams 48.2 G 50.2 G R 4 x 500 MHz channels 18.8 G 19.3 G T 2 x 250 MHz channels 19.7 G 20.2 G T 2 x 250 MHz channels ( only for 3 HEO satellites) 37.5 G 40.0 G T Gateway/ Hub applications - 5 x 500 MHz channels 40.0 G 42.0 G T 4 x 500 MHz channels S3. ORBITAL INFORMATION FOR GEOSTATIONARY SATELLITES ONLY:

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: 7 S4c. Celestial Reference Body (Earth, Sun, Moon, etc.): E S4b. Total Number of Orbital Planes in Network or System: 4 S4d. Orbit Epoch Date: 1/1/2000 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 1 1 63.4 43064 39352 1111 0 270 120 250 2 1 63.4 43064 39352 1111 120 270 120 250 3 1 63.4 43064 39352 1111 240 270 120 250 4 4 0.05 86164 35878 35878 0 235 0 360 4 4 0.05 86164 35878 35878 0 287 0 360 4 4 0.05 86164 35878 35878 0 68.5 0 360 4 4 0.05 86164 35878 35878 0 116.5 0 360 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) 1 1 0 2 1 120 3 1 240 4 1 0 4 2 0 4 3 0 4 4 0

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) 1 S AAA

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) V1R T 53 50 0.05 30 Y 1 2 20 64 V2R T 53 50 0.05 30 Y 1 2 40 67 V3R R 54.4 51.4 0.05 30 Y 1 520 27.2 -120 30 2 K1R T 48 45 0.05 30 Y 1 2 50 63 K3R T 54 51 0.05 30 Y 1 2 50 69 K4R R 54 51 0.05 30 Y 1 504 27 -134.4 32 2 K7R T -3 -5 0.1 30 N 1 3 2 -3 K8R R -3 -5 0.1 30 N 1 1154 -33.6 -90 20 2 K2R R 46.5 43.5 0.05 30 Y 1 504 19.5 -126.7 32 2 K5R T 18.5 15.5 0.1 30 N 1 2 50 33.5 K6R R 18.5 15.5 0.1 30 N 1 504 -8.5 -123.6 32 2

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) K8R R C K8R-Rx TT&C CoPol.pdf K8R R X K8R - Rx TT&C XPol.pdf V1R T C V1R Tx CoPol.pdf -140 -130 -120 -120 -120 V1R T X V1R Tx XPol.pdf V2R T C V2R Tx CoPol.pdf -131 -121 -111 -111 -111 V2R T X V2R Tx XPol.pdf V3R R C V3 Rx CoPol.pdf V3R R X V3 Rx XPol.pdf K1R T X K1R Tx 48 XPol.pdf K1R T C K1R Tx 48 CoPol.pdf -119 -118 -117 -117 -117 K2R R X K2R-Rx 46.5 Xpol.pdf K2R R C K2 Rx 46.5 CoPol.pdf K3R T C K3R Tx 54 CoPol.pdf -117 -113.7 -112.65 -109.1 -108.5 K3R T X K3R- Tx 54 XPol.pdf K4R R C K4R Rx 54 CoPol.pdf K4R R X K4R Rx 54 XPol.pdf K5R T C K5R-Tx Beacon CoPol.pdf -119.2 -119 -118.8 -118.6 -118.6 K5R T X K5R-Tx Beacon XPol.pdf K6R R C K6R-Rx Beacon CoPol.pdf K7R T C K7R-Tx-TT&C CoPol.pdf -139.4 -139.2 -139 -138.8 -138.6 K7R T X K7R-Tx-TT&C XPol.pdf K8R R C K8R-Rx TT&C CoPol.pdf K8R R X K8R - Rx TT&C XPol.pdf V1R T C V1R Tx CoPol.pdf -140 -130 -120 -120 -120 V1R T X V1R Tx XPol.pdf V2R T C V2R Tx CoPol.pdf -131 -121 -111 -111 -111 V2R T X V2R Tx XPol.pdf V3R R C V3 Rx CoPol.pdf

V3R R X V3 Rx XPol.pdf K1R T X K1R Tx 48 XPol.pdf K1R T C K1R Tx 48 CoPol.pdf -119 -118 -117 -117 -117 K2R R X K2R-Rx 46.5 Xpol.pdf K2R R C K2 Rx 46.5 CoPol.pdf K3R T C K3R Tx 54 CoPol.pdf -117 -113.7 -112.65 -109.1 -108.5 K3R T X K3R- Tx 54 XPol.pdf K4R R C K4R Rx 54 CoPol.pdf K4R R X K4R Rx 54 XPol.pdf K5R T C K5R-Tx Beacon CoPol.pdf -119.2 -119 -118.8 -118.6 -118.6 K5R T X K5R-Tx Beacon XPol.pdf K6R R C K6R-Rx Beacon CoPol.pdf K7R T C K7R-Tx-TT&C CoPol.pdf -139.4 -139.2 -139 -138.8 -138.6 K7R T X K7R-Tx-TT&C XPol.pdf

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) K1 110000 R 28662.5 L C K1 110000 R 286625 R C K2 125000 R 28787.5 L C K2 125000 R 28787.5 R C K3 125000 R 28912.5 L C K3 125000 R 28912.5 R C K4 110000 R 29037.5 L C K4 110000 R 29037.5 R C K5 125000 R 29562.5 L C K5 125000 R 29562.5 R C K6 125000 R 29687.5 L C K6 125000 R 29687.5 R C K7 125000 R 29812.5 L C K7 125000 R 29812.5 R C K8 125000 R 29937.5 L C K8 125000 R 29937.5 R C V1 300000 R 47350 L C V1 300000 R 47350 R C V2 400000 R 47700 L C V2 400000 R 47700 R C V3 300000 R 48050 L C V3 300000 R 48050 R C V4 500000 R 48450 L C V4 500000 R 48450 R C V5 500000 R 48950 L C V5 500000 R 48950 R C V6 500000 R 49450 L C V6 500000 R 49450 R C V7 500000 R 49950 R C V7 500000 R 49950 L C

B1 1000 R 29096 R C T1 2000 R 29098 R T K1T 240000 T 18925 R C K1T 240000 T 18925 L C K2T 240000 T 19175 L C K2T 240000 T 19175 R C K3T 250000 T 19825 L C K3T 250000 T 19825 R C K4T 250000 T 20075 L C K4T 250000 T 20075 R C V1T 500000 T 37750 L C V1T 500000 T 37750 R C V2T 500000 T 38250 L C T2 2000 R 28602 R T T4 2000 T 18802 L T V2T 500000 T 38250 R C V3T 500000 T 38750 L C V3T 500000 T 38750 R C V4T 500000 T 39250 L C V4T 500000 T 39250 R C V5T 500000 T 39750 L C V5T 500000 T 39750 R C V6T 500000 T 40250 L C V6T 500000 T 40250 R C V7T 500000 T 40750 L C V7T 500000 T 40750 R C V8T 500000 T 41250 L C V8T 500000 T 41250 R C V9T 500000 T 41750 L C V9T 500000 T 41750 L C B2 1000 T 19296 L C T3 2000 T 19298 L T

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) D01 7M00G7W 700 4 10100 0.9 9.3 21.3 D02 3M50G7W 3500 4 2520 0.4 7.1 19.1 D03 700KG7W 700 4 500 0.4 7.1 19.1 D04 491MG7W 491000 4 706000 0.9 9.3 21.3 D05 175MG7W 175000 4 252000 0.9 9.3 21.3 D06 87M8G7W 87800 4 63000 0.4 7.1 19.1 D07 35M1G7W 35100 4 25000 0.4 7.1 19.1 D08 10K7G7D 10.7 4 5 0.4 4.2 16.2 D09 250MG7W 250000 8 374000 0.75 8.6 20.6 D10 250MG7W 250000 4 224000 0.67 5.4 17.6 D11 250MG7W 250000 4 149000 0.45 4.2 16.4 D12 125MG7W 125000 4 112000 0.67 5.4 17.6 D13 125MG7W 125000 4 74000 0.45 4.2 16.4 D14 500MG7W 500000 8 748000 0.75 8.6 20.8 D15 334KG7D 334 4 200 0.4 4.2 16.4 D16 2M00G7D 2000 2 1000 1 15 27 D17 1M00G7D 1000 2 500 1 15 27 D18 60M0G7W 60000 8 89000 0.75 8.6 20.6 D19 60M0G7W 60000 4 53000 0.67 5.4 17.6

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 4K00F9D 4 18 27

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)

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): No Remote Control (TT C) Location(s): S14a: Street Address: TBD S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: TBD USA 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 2508 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 0 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3154 4.8 0.78 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 646 2.5 0.93 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 38 2.5 0.72 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): 8600 8170 7050 6696 Bus (Watts): (b): (g): (l): (q): 2100 2000 1720 1639 Total (Watts): (c): (h): (m): (r): 10700 10170 8770 8335 Solar Array (Watts): (d): (i): (n): (s): 11200 10670 9180 8745 Depth of Battery (e) (j) (o) (t) Discharge (%): 70 % 70 % 70 % 70 % 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: 2007-02-26 17:11:27
Document Modified: 2007-02-26 17:11:27
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