Attachment Schedule S Tech Data

This document pretains to SAT-LOI-20080910-00178 for Letter of Intent on a Satellite Space Stations filing.

IBFS_SATLOI2008091000178_663888

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: BSSNET119W 12/30/2012 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 6/30/2009 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 10/30/2011 154 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: 12/30/2011 12/30/2011 3696 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) 17.3 G 17.7 G T Broadcasting Satellite Service - Data 17.3 G 17.7 G T Broadcasting Satellite Service - Sound 17.3 G 17.7 G T Broadcasting Satellite Service - Video 17.3 G 17.7 G T TTC 24.75 G 25.15 G R Broadcasting Satellite Service - Data 24.75 G 25.15 G R Broadcasting Satellite Service - Sound 24.75 G 25.15 G R Broadcasting Satellite Service - Video 24.75 G 25.15 G R TTC 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: 119 W Available Appendix F orbital location Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be 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 USA, HWA, ALS NESPOT S USA, North of 38N, East of 100WL SESPOT S USA, South of 38N, East of 100WL WSPOT S USA, West of 100 WL HISPOT S HWA LAUL S ULLA SA.gxt Sample spot LA Uplink CMD S USA

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) USA T 36.5 27.7 0.1 30 N CONUS+ 2.5 318 61.4 SP28 T 46.5 44.5 0.1 30 N NESPOT 2.5 16.5 58.7 SP48 T 46.5 44.5 0.1 30 N SESPOT 2.5 30.7 61.4 SP31 T 46.5 44.5 0.1 30 N WSPOT 2.5 17.3 55.1 SP50 T 46.5 44.5 0.1 30 N HISPOT 2.5 15.2 58.3 LAUL R 47 46 0.1 30 N LAUL 794 17.5 -109 20 1 CMD R 19 0.1 30 N CMD 645 -9.1 LAUL

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) USA T C -119 119 Conus.gxt -122.9 -122.9 -122.9 -124.9 -123.9 SP28 T C -119 SP28.gxt -124.1 -124.1 -124.1 -126.1 -125.1 SP48 T C -119 SP48.gxt -124.1 -124.1 -124.1 -126.1 -125.1 SP31 T C -119 SP31.gxt -124.1 -124.1 -124.1 -126.1 -125.1 SP50 T C -119 SP50.gxt -124.1 -124.1 -124.1 -126.1 -125.1 LAUL R C -119 ULLA G.gxt CMD R C -119 CMD2.gxt

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) FA001 24000 T 17325 L C NA001 156 GA001 LAUL FA001 USA FA003 24000 T 17354.16 L C NA002 156 GA003 LAUL FA003 USA FA005 24000 T 17383.32 L C NA003 156 GA005 LAUL FA005 USA FA007 24000 T 17412.48 L C NA004 156 GA007 LAUL FA007 USA FA009 24000 T 17441.64 L C NA005 156 GA009 LAUL FA009 USA FA011 24000 T 17470.8 L C NB001 156 GB002 LAUL FB002 USA FA013 24000 T 17499.96 L C NB002 156 GB004 LAUL FB004 USA FA015 24000 T 17529.12 L C NB003 156 GB006 LAUL FB006 USA FA017 24000 T 17558.28 L C NB004 156 GB008 LAUL FB008 USA FA019 24000 T 17587.44 L C NB005 156 GB010 LAUL FB010 USA FA021 24000 T 17616.6 L C SA001 156 GA011 LAUL FA011 SP28 FA023 24000 T 17645.76 L C SA002 156 GA013 LAUL FA013 SP28 FA025 24000 T 17674.92 L C SA003 156 GA015 LAUL FA015 SP28 FB002 24000 T 17325 R C SA004 156 GA017 LAUL FA017 SP28 FB004 24000 T 17354.16 R C SA005 156 GA019 LAUL FA019 SP28 FB006 24000 T 17383.32 R C SA006 156 GA021 LAUL FA021 SP28 FB008 24000 T 17412.48 R C SA007 156 GA023 LAUL FA023 SP28 FB010 24000 T 17441.64 R C SA008 156 GA025 LAUL FA025 SP28 FB012 24000 T 17470.8 R C SA009 156 GA011 LAUL FA011 SP48 FB014 24000 T 17499.96 R C SA010 156 GA013 LAUL FA013 SP48 FB016 24000 T 17529.12 R C SA011 156 GA015 LAUL FA015 SP48 FB018 24000 T 17558.28 R C SA012 156 GA017 LAUL FA017 SP48 FB020 24000 T 17587.44 R C SA013 156 GA019 LAUL FA019 SP48 FB022 24000 T 17616.6 R C SA014 156 GA021 LAUL FA021 SP48 FB024 24000 T 17645.76 R C SA015 156 GA023 LAUL FA023 SP48 FB026 24000 T 17674.92 R C SA016 156 GA025 LAUL FA025 SP48 GA001 24000 R 24775 R C SA017 156 GA011 LAUL FA011 SP31 GA003 24000 R 24804.16 R C SA018 156 GA013 LAUL FA013 SP31 GA005 24000 R 24833.32 R C SA019 156 GA015 LAUL FA015 SP31 GA007 24000 R 24862.48 R C SA020 156 GA017 LAUL FA017 SP31

GA009 24000 R 24891.64 R C SA021 156 GA019 LAUL FA019 SP31 GA011 24000 R 24920.8 R C SA022 156 GA021 LAUL FA021 SP31 GA013 24000 R 24949.96 R C SA023 156 GA023 LAUL FA023 SP31 GA015 24000 R 24979.12 R C SA024 156 GA025 LAUL FA025 SP31 GA017 24000 R 25008.28 R C SA025 156 GA011 LAUL FA011 SP50 GA019 24000 R 25037.44 R C SA026 156 GA013 LAUL FA013 SP50 GA021 24000 R 25066.6 R C SA027 156 GA015 LAUL FA015 SP50 GA023 24000 R 25095.76 R C SA028 156 GA017 LAUL FA017 SP50 GA025 24000 R 25124.92 R C SA029 156 GA019 LAUL FA019 SP50 GB002 24000 R 24775 L C SA030 156 GA021 LAUL FA021 SP50 GB004 24000 R 24804.16 L C SA031 156 GA023 LAUL FA023 SP50 GB006 24000 R 24833.32 L C SA032 156 GA025 LAUL FA025 SP50 GB008 24000 R 24862.48 L C SB001 156 GB012 LAUL FB012 SP28 GB010 24000 R 24891.64 L C SB002 156 GB014 LAUL FB014 SP28 GB012 24000 R 24920.8 L C SB003 156 GB016 LAUL FB016 SP28 GB014 24000 R 24949.96 L C SB004 156 GB018 LAUL FB018 SP28 GB016 24000 R 24979.12 L C SB005 156 GB020 LAUL FB020 SP28 GB018 24000 R 25008.28 L C SB006 156 GB022 LAUL FB022 SP28 GB020 24000 R 25037.44 L C SB007 156 GB024 LAUL FB024 SP28 GB022 24000 R 25066.6 L C SB008 156 GB026 LAUL FB026 SP28 GB024 24000 R 25095.76 L C SB009 156 GB012 LAUL FB012 SP48 GB026 24000 R 25124.92 L C SB010 156 GB014 LAUL FB014 SP48 CMD1 1000 R 24765 L T SB011 156 GB016 LAUL FB016 SP48 TLM1 1000 T 17695 L T SB012 156 GB018 LAUL FB018 SP48 BEA1 10 T 17693 L T SB013 156 GB020 LAUL FB020 SP48 SB014 156 GB022 LAUL FB022 SP48 SB015 156 GB024 LAUL FB024 SP48 SB016 156 GB026 LAUL FB026 SP48 SB017 156 GB012 LAUL FB012 SP31 SB018 156 GB014 LAUL FB014 SP31 SB019 156 GB016 LAUL FB016 SP31 SB020 156 GB018 LAUL FB018 SP31 SB021 156 GB020 LAUL FB020 SP31 SB022 156 GB022 LAUL FB022 SP31 SB023 156 GB024 LAUL FB024 SP31 SB024 156 GB026 LAUL FB026 SP31 SB025 156 GB012 LAUL FB012 SP50 SB026 156 GB014 LAUL FB014 SP50 SB027 156 GB016 LAUL FB016 SP50

SB028 156 GB018 LAUL FB018 SP50 SB029 156 GB020 LAUL FB020 SP50 SB030 156 GB022 LAUL FB022 SP50 SB031 156 GB024 LAUL FB024 SP50 SB032 156 GB026 LAUL FB026 SP50 C1 CMD1 CMD B1 BEA1 SP28

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 24M0G7W 24000 8 42800 0.66 6.6 20 C1 1M00F2D 1000 37.4 49.6 B1 H001N0N 10 20.5 32.7

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)

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) NA001 NB005 D1 1 Comm Link.doc 67.6 0 8 52.6 61.4 -115 17.2 SA001 SB032 D1 1 Comm Link.doc 67.6 0 8 51.2 61.4 -115 17.2 C1 C1 C1 1 TTC Link.doc 63.4 17 27 B1 B1 B1 1 TTC Link.doc 45.4 -20 -20 25.4 25.4 -137 16.3

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: S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Curacao 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 3905 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2684 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6595 50 0.6 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 293 8.2 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 85 7.3 0.51 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): 15860 15860 15860 15860 Bus (Watts): (b): (g): (l): (q): 1800 700 1800 700 Total (Watts): (c): (h): (m): (r): 17856 16533 17856 16533 Solar Array (Watts): (d): (i): (n): (s): 21653 19690 18590 17279 Depth of Battery (e) (j) (o) (t) Discharge (%): 79.5 % 0 % 79.5 % 0 % 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: 2008-09-12 11:46:46
Document Modified: 2008-09-12 11:46:46
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