Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20060425-00047 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2006042500047_498205

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: GALAXY-9 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 24 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: 864 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) 5925 M 6425 M R Fixed Satellite Service 3700 M 4200 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: 74.15 W Provide C-band service to the United States 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) 1 S United States 2 S Global

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) CHU R 33.1 27.1 0.2 0.19 33 Y 01 4.7 -93 14 2 CVU R 30.6 24.6 0.2 0.19 33 Y 90 1 3.4 -91.7 14 2 CHD T 29.9 25.9 0.2 0.19 33 Y 01 40.8 CVD T 29.4 25.4 0.2 0.19 33 Y 90 1 42 OCM R 3.8 2.8 0.2 0.19 N 2 -25.8 OTL T 2.9 1.9 0.2 0.19 N 2 7.9

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) CHU R C 74.15 CHUP.gxt CVU R C 74.15 CVUP.gxt CHD T C 74.15 CHDN.gxt -152 -151.2 -151 -150.9 -150.8 CVD T C 74.15 CVDN.gxt -152 -151.2 -151 -150.9 -150.8 OCM R C 74.15 OCMD.PDF OTL T C 74.15 OTLM.PDF -170.1 -170 -169.9 -169.8 -169.7

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) UC1 36000 R 5945 V C 1C 111.8 UC1 CVUP DC1 CHDN UC3 36000 R 5985 V C 3C 111.8 UC3 CVUP DC3 CHDN UC5 36000 R 6025 V C 5C 111.8 UC5 CVUP DC5 CHDN UC7 36000 R 6065 V C 7C 111.8 UC7 CVUP DC7 CHDN UC9 36000 R 6105 V C 9C 111.8 UC9 CVUP DC9 CHDN UC11 36000 R 6145 V C 11C 111.8 UC11 CVUP DC11 CHDN UC13 36000 R 6185 V C 13C 111.8 UC13 CVUP DC13 CHDN UC15 36000 R 6225 V C 15C 111.8 UC15 CVUP DC15 CHDN UC17 36000 R 6265 V C 17C 111.8 UC17 CVUP DC17 CHDN UC19 36000 R 6305 V C 19C 111.8 UC19 CVUP DC19 CHDN UC21 36000 R 6345 V C 21C 111.8 UC21 CVUP DC21 CHDN UC23 36000 R 6385 V C 23C 111.8 UC23 CVUP DC23 CHDN UC2 36000 R 5965 H C 2C 107.3 UC2 CHUP DC2 CVDN UC4 36000 R 6005 H C 4C 107.3 UC4 CHUP DC4 CVDN UC6 36000 R 6045 H C 6C 107.3 UC6 CHUP DC6 CVDN UC8 36000 R 6085 H C 8C 107.3 UC8 CHUP DC8 CVDN UC10 36000 R 6125 H C 10C 107.3 UC10 CHUP DC10 CVDN UC12 36000 R 6165 H C 12C 107.3 UC12 CHUP DC12 CVDN UC14 36000 R 6205 H C 14C 107.3 UC14 CHUP DC14 CVDN UC16 36000 R 6245 H C 16C 107.3 UC16 CHUP DC16 CVDN UC18 36000 R 6285 H C 18C 107.3 UC18 CHUP DC18 CVDN UC20 36000 R 6325 H C 20C 107.3 UC20 CHUP DC20 CVDN UC22 36000 R 6365 H C 22C 107.3 UC22 CHUP DC22 CVDN UC24 36000 R 6405 H C 24C 107.3 UC24 CHUP DC24 CVDN DC1 36000 T 3720 H C DC3 36000 T 3760 H C DC5 36000 T 3800 H C DC7 36000 T 3840 H C DC9 36000 T 3880 H C DC11 36000 T 3920 H C

DC13 36000 T 3960 H C DC15 36000 T 4000 H C DC17 36000 T 4040 H C DC19 36000 T 4080 H C DC21 36000 T 4120 H C DC23 36000 T 4160 H C DC2 36000 T 3740 V C DC4 36000 T 3780 V C DC6 36000 T 3820 V C DC8 36000 T 3860 V C DC10 36000 T 3900 V C DC12 36000 T 3940 V C DC14 36000 T 3980 V C DC16 36000 T 4020 V C DC18 36000 T 4060 V C DC20 36000 T 4100 V C DC22 36000 T 4140 V C DC24 36000 T 4180 V C CMD1 1000 R 6424.5 V T CMD2 1000 R 5925.5 H T TLM1 500 T 4199 H T TLM2 500 T 4199.875 H T TLM3 500 T 4199 V T TLM4 500 T 4199.875 V 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) D1 30M1G7W 30133 4 36863 0.75 6.1 15.7 D2 4M15G7W 4154 4 6000 0.75 6.7 14 D3 1M21G7W 1212.8 4 1550 0.75 5.7 12.9 D4 75K4G7W 75.4 4 64 0.5 3 12.1

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 36M0F3F 36000 TV/FM 1 NTSC 12.8 2.56 10 17

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) 1C 23C A1 1 GXY9-LINK BU 4000 52.8 18.4 24.4 36.8 40.8 -151.3 23.6 1C 23C D1 1 GXY9-LINK BU 52.8 18.4 24.4 36.8 40.8 -160.1 21 1C 23C D2 3 6875 GXY9-LINK BU 52.8 6.9 12.9 26.7 30.7 -161.5 21 1C 23C D3 15 1550 GXY9-LINK BU 52.8 0.4 6.4 20.2 24.2 -162.7 21 1C 23C D4 239 100 GXY9-LINK BU 52.8 -11.4 -5.4 8.4 12.4 -162.4 19.2 2C 24C A1 1 GXY9-LINK BU 4000 52.8 17.1 23.1 38 42 -150.1 23.6 2C 24C D1 1 GXY9-LINK BU 52.8 17.1 23.1 38 42 -158.8 19.2 2C 24C D2 3 6875 GXY9-LINK BU 52.8 3.3 9.3 27.6 31.6 -160.6 21 2C 24C D3 16 1550 GXY9-LINK BU 52.8 -3.1 2.9 21.2 25.2 -161.7 21 2C 24C D4 273 100 GXY9-LINK BU 52.8 -15.3 -9.3 9 13 -161.8 19.2

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): #Error

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 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: S16. SPACECRAFT ELECTRICAL CHARACTERISTICS: 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: 2006-05-02 12:29:50
Document Modified: 2006-05-02 12:29:50
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