Attachment Schedule S Tech Data

This document pretains to SAT-AMD-20080118-00029 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2008011800029_617383

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: PEGASUS 91W N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 32 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: 768 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 - Video 17.3 G 17.7 G T Broadcasting Satellite Service - Sound 17.3 G 17.7 G T Broadcasting Satellite Service - Data 24.75 G 25.15 G R Feeder Link for Broadcasting Satellite Service in FSS 17.7 G 17.8 G T Broadcasting Satellite Service - Video 17.7 G 17.8 G T Broadcasting Satellite Service - Sound 17.7 G 17.8 G T Broadcasting Satellite Service - Data 25.15 G 25.25 G R Feeder Link for Broadcasting Satellite Service in FSS 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: 91 W good elevation angle for subscribers in all coverage Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be areas 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) CONUST S CONUS + AK + HI + PR CONUSR E CONUS MEXT S Mexico

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) CON T 37.1 27.1 0.1 0.05 25 N CONUST 4 204.2 60.2 CON R 33.1 23.1 0.1 0.05 25 N CONUSR 912 3.5 -100 20 1 CON T 37.1 27.1 0.1 0.05 25 N CONUST 4 204.2 60.2 CON R 33.1 23.1 0.1 0.05 25 N CONUSR 912 3.5 -100 20 1 MEX T 37 27 0.1 0.05 25 N MEXT 1 100 57.1 MEX T 37 27 0.1 0.05 25 N MEXT 1 100 57.1

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 -91 CONTRfig -123.3 -123.3 -123.3 -123.3 -123.3 CON R C -91 CONRR fig CON T C -91 CONTL fig -123.3 -123.3 -123.3 -123.3 -123.3 CON R C -91 CONRL fig MEX T C -91 MEXTR fig -126.4 -126.4 -126.4 -126.4 -126.4 MEX T C -91 MEXTL fig -126.4 -126.4 -126.4 -126.4 -126.4

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) C24R 24000 R 25096.34 L C T1 139.7 C1R CONRR C1T CONTR C25T 24000 T 17675.50 R C T2 139.7 C2R CONRL C2T CONTL C25R 24000 R 25125.50 R C T3 139.7 C3R CONRR C3T CONTR C26T 24000 T 17675.50 L C T4 139.7 C4R CONRL C4T CONTL C26R 24000 R 25125.50 L C T5 139.7 C5R CONRR C5T CONTR BEA 1000 T 17695.00 R T T6 139.7 C6R CONRL C6T CONTL M27T 24000 T 17721.08 R C T7 139.7 C7R CONRR C7T CONTR M27R 24000 R 25171.08 R C T8 139.7 C8R CONRL C8T CONTL M28T 24000 T 17721.08 L C T9 139.7 C9R CONRR C9T CONTR M28R 24000 R 25171.08 L C T10 139.7 C10R CONRL C10T CONTL M29T 24000 T 17750.24 R C T11 139.7 C11R CONRR C11T CONTR M29R 24000 R 25200.24 R C T12 139.7 C12R CONRL C12T CONTL M30T 24000 T 17750.24 L C T13 139.7 C13R CONRR C13T CONTR M30R 24000 R 25200.24 L C T14 139.7 C14R CONRL C14T CONTL M31T 24000 T 17779.40 R C T15 139.7 C15R CONRR C15T CONTR M31R 24000 R 25229.40 R C T16 139.7 C16R CONRL C16T CONTL M32T 24000 T 17779.40 L C T17 139.7 C17R CONRR C17T CONTR M32R 24000 R 25229.40 L C T18 139.7 C18R CONRL C18T CONTL TEL 316 T 17303.00 R T T19 139.7 C19R CONRR C19T CONTR COM 2000 R 24755.00 R T T20 139.7 C20R CONRL C20T CONTL C1T 24000 T 17325.58 R C T21 139.7 C21R CONRR C21T CONTR C1R 24000 R 24775.00 R C T22 139.7 C22R CONRL C22T CONTL C2T 24000 T 17325.58 L C T23 139.7 C23R CONRR C23T CONTR C2R 24000 R 24775.00 L C T24 139.7 C24R CONRL C24T CONTL C3T 24000 T 17254.74 R C T25 139.7 C25R CONRR C25T CONTR C3R 24000 R 24804.74 R C T26 139.7 C26R CONRL C26T CONTL C4T 24000 T 17254.74 L C T27 136.7 M27R CONRR M27T MEXTR C4R 24000 R 24804.74 L C T28 136.7 M28R CONRL M28T MEXTL C5T 24000 T 17383.90 R C T29 136.7 M29R CONRR M29T MEXTR C5R 24000 R 24833.90 R C T30 136.7 M30R CONRL M30T MEXTL

C6T 24000 T 17383.9 L C T31 136.7 M31R CONRR M31T MEXTR C6R 24000 R 24833.90 L C T32 136.7 M32R CONRL M32T MEXTL C7T 24000 T 17413.06 R C TTEL TEL CONTR C7R 24000 R 24863.06 R C TCOM COM CONRR C8T 24000 T 17413.06 L C TBEA BEA CONTR C8R 24000 R 24863.06 L C C9T 24000 T 17442.22 R C C9R 24000 R 24892.22 R C C10T 24000 T 17442.22 L C C10R 24000 R 24982.22 L C C11T 24000 T 17471.38 R C C11R 24000 R 24921.38 R C C12T 24000 T 17471.38 L C C12R 24000 R 24921.38 L C C13T 24000 T 17500.54 R C C13R 24000 R 24950.54 R C C14T 24000 T 17500.54 L C C14R 24000 R 24950.54 L C C15T 24000 T 17529.70 R C C15R 24000 R 24979.70 R C C16T 24000 T 17529.70 L C C16R 24000 R 24979.70 L C C17T 24000 T 17558.86 R C C17R 24000 R 25008.86 R C C18T 24000 T 17558.86 L C C18R 24000 R 25008.86 L C C19T 24000 T 17588.02 R C C19R 24000 R 25038.02 R C C20T 24000 T 17588.02 L C C20R 24000 R 25038.02 L C C21T 24000 T 17617.18 R C C21R 24000 R 25067.18 R C C22T 24000 T 17617.18 L C C22R 24000 R 25067.18 L C C23T 24000 T 17646.34 R C C23R 24000 R 25096.34 R C C24T 24000 T 17646.34 L C

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) 1 24M0G1W 24000 4 25600 0.64 4 22 2 24M0G1W 24000 4 28400 0.71 4.8 22 3 24M0G1W 24000 8 38400 0.64 7.6 22 4 24M0G1W 24000 8 42300 0.71 9 22 5 1K00N0N 1000 1 8 22 6 350KG9D 350 8 22 7 2M00G2D 2000 8 22

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) T1 T26 1 1 see attached 59.8 23.3 33.3 50.2 60.2 -115.1 11.2 T1 T26 2 1 see attached 59.8 23.3 33.3 50.2 60.2 -115.1 11.2 T1 T26 3 1 see attached 59.8 23.3 33.3 50.2 60.2 -115.1 11.2 T1 T26 4 1 see attached 59.8 23.3 33.3 50.2 60.2 -115.1 11.2 T27 T32 1 1 see attached 59.8 23.3 33.3 47.1 57.1 -118.2 11.2 T27 T32 2 1 see attached 59.8 23.3 33.3 47.1 57.1 -118.2 11.2 T27 T32 3 1 see attached 59.8 23.3 33.3 47.1 57.1 -118.2 11.2 T27 T32 4 1 see attached 59.8 23.3 33.3 47.1 57.1 -118.2 11.2 TTEL TTEL 6 1 see attached 15 20 -137.8 37.3 TBEA TBEA 5 1 see attached 11 11 -151.4 37.3 TCOM TCOM 7 1 see attached 59.8 5.2 25.2

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: TBD S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: 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 3000 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3200 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6200 32.5 0.87 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 740 8 0.87 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 90 8.2 0.75 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): 13800 13800 13800 13800 Bus (Watts): (b): (g): (l): (q): 3500 1650 3500 1650 Total (Watts): (c): (h): (m): (r): 17300 15450 17300 15540 Solar Array (Watts): (d): (i): (n): (s): 21700 19350 19100 17150 Depth of Battery (e) (j) (o) (t) Discharge (%): 70 % 0 % 70 % 15 % 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: 2008-01-22 13:06:56
Document Modified: 2008-01-22 13:06:56
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