Attachment Schedule S Tech Data

This document pretains to SES-MFS-20060811-01347 for Modification w/ Foreign Satellite (earth station) on a Satellite Earth Station filing.

IBFS_SESMFS2006081101347_519124

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: WB-1 1/30/2007 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 11/2/1999 12 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 3/15/2005 41 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: 11/15/2006 12/15/2006 6000 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) 28.35 G 28.6 G R Fixed Satellite Service 29.25 G 30 G R Fixed Satellite Service 18.3 G 18.8 G T Fixed Satellite Service 19.7 G 20.2 G T Fixed Satellite Service 5859.0 M 5860.0 M R Fixed Satellite Service 6423.0 M 6424.0 M R Fixed Satellite Service 3701.4 M 3701.6 M T Fixed Satellite Service 4197.9 M 4198.1 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: 111.1 W This orbital location provides high elevation angles Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be over all of CONUS. High elevation satellite visibility is N/S Station-Keeping provided (Optional): important for a satellite network providing services d. Toward West: Degrees E/W 0.05 Degrees Tolerance: directly to subscriber terminals, and operating at Ka- g. Westernmost: e. Toward East: 0.05 Degrees band frequencies where rain attenuation effects are 0.05 Degrees h. Easternmost: significant and elevation angle dependent. 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) NORTH_AMER S North America GLOBAL S Visible Earth.

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) KSD1 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD2 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.7 26.3 60.4 KSD3 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.5 20.9 59.4 KSD4 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.7 26.3 60.4 OMN R 0 -4 0.085 0.085 30 N 90 GLOBAL 1000 -30 OMN T 0 -4 0.085 0.085 30 N 0 GLOBAL 4.4 8.9 9.5 TLML T 28 24 0.085 0.085 30 N NORTH_A 3.6 0.09 17 OMN R 0 -4 0.085 0.085 30 N 0 GLOBAL 1000 -30 OMN T 0 -4 0.085 0.085 30 N 90 GLOBAL 4.4 8.9 9.5 KSD5 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.7 26.3 60.4 KSD6 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.7 26.3 60.4 KSD8 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.7 26.3 60.4 KSD9 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.8 61.7 64.1 KSD1 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.7 26.3 60.4 KSD1 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.8 61.7 64.1 KSD1 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.8 61.7 64.1 KSD1 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD1 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD1 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD1 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD1 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD1 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD1 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.5 20.9 59.4 KSD2 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.8 61.7 64.1 KSD2 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD2 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.7 26.3 60.4 KSD2 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD2 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD2 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6

KSD2 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD2 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD2 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.8 61.7 64.1 KSD2 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.8 61.7 64.1 KSD3 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.7 26.3 60.4 KSD3 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.7 26.3 60.4 KSD3 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.7 26.3 60.4 KSD3 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.7 26.3 60.4 KSD3 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.5 87.1 65.6 KSD3 T 46.2 42.2 0.085 0.085 27 N NORTH_A 3.7 26.3 60.4 KSD3 T 46.2 42.2 0.085 0.085 27 N NORTH_A 1.8 61.7 64.1 KSU1 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU2 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU3 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU4 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU5 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU6 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU8 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU9 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU1 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU1 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU1 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU1 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU1 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU1 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU1 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU1 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU1 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU1 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU2 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU2 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU2 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU2 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU2 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU2 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU2 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU2 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU2 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU2 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1

KSU3 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU3 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU3 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU3 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU3 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU3 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KSU3 R 46.2 42.2 0.085 0.085 27 N NORTH_A 690 17.8 -103 31 1 KGU R 45.8 41.8 0.085 0.085 27 N NORTH_A 950 16 -103 12 0.5 KGU R 45.8 41.8 0.085 0.085 27 N NORTH_A 950 16 -103 12 0.5 KGU R 45.8 41.8 0.085 0.085 27 N NORTH_A 950 16 -103 12 0.5 KGU R 45.8 41.8 0.085 0.085 27 N NORTH_A 950 16 -103 12 0.5 KGU R 45.8 41.8 0.085 0.085 27 N NORTH_A 950 16 -103 12 0.5 KGU R 45.8 41.8 0.085 0.085 27 N NORTH_A 950 16 -103 12 0.5 KGD T 45.2 41.2 0.085 0.085 27 N NORTH_A 3.6 40.7 61.3 KGD T 45.2 41.2 0.085 0.085 27 N NORTH_A 3.6 40.7 61.3 KGD T 45.2 41.2 0.085 0.085 27 N NORTH_A 3.6 40.7 61.3 KGD T 45.2 41.2 0.085 0.085 27 N NORTH_A 3.6 40.7 61.3 KGD T 45.2 41.2 0.085 0.085 27 N NORTH_A 3.6 40.7 61.3 KGD T 45.2 41.2 0.085 0.085 27 N NORTH_A 3.6 40.7 61.3

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) KSD1 T C -111.1 KSD1.gxt -118 -118 -118 -118 -118 KSD2 T C -111.1 KSD2.gxt -118 -118 -118 -118 -118 KSD3 T C -111.1 KSD3.gxt -118 -118 -118 -118 -118 KSD4 T C -111.1 KSD4.gxt -118 -118 -118 -118 -118 KSD5 T C -111.1 KSD5.gxt -118 -118 -118 -118 -118 KSD6 T C -111.1 KSD6.gxt -118 -118 -118 -118 -118 KSD8 T C -111.1 KSD8.gxt -118 -118 -118 -118 -118 KSD9 T C -111.1 KSD9.gxt -118 -118 -118 -118 -118 KSD1 T C -111.1 KSD10.gxt -118 -118 -118 -118 -118 KSD1 T C -111.1 KSD11.gxt -118 -118 -118 -118 -118 KSD1 T C -111.1 KSD12.gxt -118 -118 -118 -118 -118 KSD1 T C -111.1 KSD13.gxt -118 -118 -118 -118 -118 KSD1 T C -111.1 KSD14.gxt -118 -118 -118 -118 -118 KSD1 T C -111.1 KSD15.gxt -118 -118 -118 -118 -118 KSD1 T C -111.1 KSD16.gxt -118 -118 -118 -118 -118 KSD1 T C -111.1 KSD17.gxt -118 -118 -118 -118 -118 KSD1 T C -111.1 KSD18.gxt -118 -118 -118 -118 -118 KSD1 T C -111.1 KSD19.gxt -118 -118 -118 -118 -118 KSD2 T C -111.1 KSD20.gxt -118 -118 -118 -118 -118 KSD2 T C -111.1 KSD21.gxt -118 -118 -118 -118 -118 KSD2 T C -111.1 KSD22.gxt -118 -118 -118 -118 -118 KSD2 T C -111.1 KSD23.gxt -118 -118 -118 -118 -118 KSD2 T C -111.1 KSD24.gxt -118 -118 -118 -118 -118 KSD2 T C -111.1 KSD25.gxt -118 -118 -118 -118 -118 KSD2 T C -111.1 KSD26.gxt -118 -118 -118 -118 -118 KSD2 T C -111.1 KSD27.gxt -118 -118 -118 -118 -118 KSD2 T C -111.1 KSD28.gxt -118 -118 -118 -118 -118 KSD2 T C -111.1 KSD29.gxt -118 -118 -118 -118 -118

KSD3 T C -111.1 KSD30.gxt -118 -118 -118 -118 -118 KSD3 T C -111.1 KSD31.gxt -118 -118 -118 -118 -118 KSD3 T C -111.1 KSD32.gxt -118 -118 -118 -118 -118 KSD3 T C -111.1 KSD33.gxt -118 -118 -118 -118 -118 KSD3 T C -111.1 KSD34.gxt -118 -118 -118 -118 -118 KSD3 T C -111.1 KSD35.gxt -118 -118 -118 -118 -118 KSD3 T C -111.1 KSD36.gxt -118 -118 -118 -118 -118 KSU1 R C -111.1 KSU1.gxt KSU2 R C -111.1 KSU2.gxt KSU3 R C -111.1 KSU3.gxt KSU4 R C -111.1 KSU4.gxt KSU5 R C -111.1 KSU5.gxt KSU6 R C -111.1 KSU6.gxt KSU8 R C -111.1 KSU8.gxt KSU9 R C -111.1 KSU9.gxt KSU1 R C -111.1 KSU10.gxt KSU1 R C -111.1 KSU11.gxt KSU1 R C -111.1 KSU12.gxt KSU1 R C -111.1 KSU13.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) AGU1 62500 R 28381.25 R C F1 126.5 AGU KGU1 ASD KSD1 AGU2 62500 R 28443.75 R C F2 124.3 BGU1 KGU1 BSD1 KSD2 BGU1 62500 R 28506.25 R C F3 123.3 AGU2 KGU11 ASD2 KSD3 BGU2 62500 R 28568.75 R C F4 124.3 BGU2 KGU1 BSD2 KSD4 CGU1 62500 R 29281.25 R C F5 124.3 AGU1 KGU27 ASD1 KSD5 CGU2 62500 R 29343.75 R C F6 124.3 BGU2 KGU11 BSD2 KSD6 DGU1 62500 R 29406.25 R C F8 124.3 CGU2 KGU1 CSD2 KSD8 DGU2 62500 R 29468.75 R C F9 125 DGU2 KGU1 DSD2 KSD9 ASU1 62500 R 29531.25 L C F10 124.3 CGU1 KGU1 CSD1 KSD10 ASU2 62500 R 29593.75 L C F11 125 DGU2 KGU11 DSD2 KSD11 BSU1 62500 R 29656.25 L C F12 125 CGU2 KGU27 CSD2 KSD12 BSU2 62500 R 29718.75 L C F13 126.5 DGU KGU27 DSD KSD13 CSU1 62500 R 29781.25 L C F14 126.5 CGU KGU35 CSD KSD14 CSU2 62500 R 29843.75 L C F15 126.5 DGU KGU35 DSD KSD15 DSU1 62500 R 29906.25 L C F16 126.5 CGU KGU16 CSD KSD16 DSU2 62500 R 29968.75 L C F17 126.5 DGU KGU16 DSD KSD17 AGU 125000 R 28412.50 R C F18 126.5 BGU KGU27 BSD KSD18 BGU 125000 R 28537.50 R C F19 123.3 AGU1 KGU11 ASD1 KSD19 CGU 125000 R 29312.50 R C F20 125 BGU2 KGU6 BSD2 KSD20 DGU 125000 R 29437.50 R C F21 126.5 AGU KGU6 ASD KSD21 ASU 125000 R 29562.50 L C F22 124.3 BGU1 KGU11 BSD1 KSD22 BSU 125000 R 29687.50 L C F23 126.5 AGU KGU35 ASD KSD23 CSU 125000 R 29812.50 L C F24 126.5 BGU KGU35 BSD KSD24 DSU 125000 R 29937.50 L C F25 126.5 AGU KGU16 ASD KSD25 AGD1 62500 T 18331.25 L C F26 126.5 BGU KGU16 BSD KSD26 AGD2 62500 T 18393.75 L C F27 126.5 CGU KGU11 CSD KSD27 BGD1 62500 T 18456.25 L C F28 125 DGU2 KGU1 DSD2 KSD28 BGD2 62500 T 18518.75 L C F29 125 CGU1 KGU27 CSD1 KSD29 CGD1 62500 T 18581.25 L C F30 124.3 DGU1 KGU6 DSD1 KSD30 CGD2 62500 T 18643.75 L C F31 124.3 CGU2 KGU6 CSD2 KSD31

DGD1 62500 T 18706.25 L C F32 124.3 DGU2 KGU6 DSD2 KSD32 DGD2 62500 T 18768.75 L C F33 124.3 CGU1 KGU6 CSD1 KSD33 ASD1 62500 T 19731.25 R C F34 126.5 DGU1 KGU11 DSD1 KSD34 ASD2 62500 T 19793.75 R C F35 124.3 AGU1 KGU27 ASD1 KSD35 BSD1 62500 T 19856.25 R C R1 123.9 ASU KSU1 AGD KGD1 BSD2 62500 T 19918.75 R C R2 123.9 BSU1 KSU2 BGD1 KGD1 CSD1 62500 T 19981.25 R C R3 123.9 ASU2 KSU3 AGD2 KGD11 CSD2 62500 T 20043.75 R C R4 123.9 BSU2 KSU4 BGD2 KGD1 CMD1 1000 R 29999.50 R T R5 123.9 ASU2 KSU5 AGD2 KGD27 CMD2 1000 R 5859.50 H T R6 123.9 BSU2 KSU6 BGD2 KGD11 CMD4 1000 R 6423.50 V T R8 123.9 CSU2 KSU8 CGD2 KGD1 TLM1 200 T 20196.0 L T R9 123.9 DSU2 KSU9 DGD2 KGD1 TLM2 200 T 20199.5 L T R10 123.9 CSU1 KSU10 CGD1 KGD1 TLM3 200 T 3701.5 V T R11 123.9 DSU2 KSU11 DGD2 KGD11 TLM4 200 T 4198.0 H T R12 123.9 CSU2 KSU12 CGD2 KGD27 ASD 125000 T 19762.50 R C R13 123.9 DSU KSU13 DGD KGD27 BSD 125000 T 19887.50 R C R14 123.9 CSU KSU14 CGD KGD35 CSD 125000 T 20012.50 R C R15 123.9 DSU KSU15 DGD KGD35 DSD 125000 T 20137.50 R C R16 123.9 CSU KSU16 CGD KGD16 AGD 125000 T 18362.50 L C R17 123.9 DSU KSU17 DGD KGD16 BGD 125000 T 18487.50 L C R18 123.9 BSU KSU18 BGD KGD27 CGD 125000 T 18612.50 L C R19 123.9 ASU1 KSU19 AGD1 KGD11 DGD 125000 T 18737.50 L C R20 123.9 BSU2 KSU20 BGD2 KGD6 DSD1 62500 T 20106.25 R C R21 123.9 ASU KSU21 AGD KGD6 DSD2 62500 T 20168.75 R C R22 123.9 BSU1 KSU22 BGD1 KGD11 R23 123.9 ASU KSU23 AGD KGD35 R24 123.9 BSU KSU24 BGD KGD35 R25 123.9 ASU KSU25 AGD KGD16 R26 123.9 BSU KSU26 BGD KGD16 R27 123.9 CSU KSU27 CGD KGD11 R28 123.9 DSU1 KSU28 DGD1 KGD1 R29 123.9 CSU1 KSU29 CGD1 KGD27 R30 123.9 DSU1 KSU30 DGD1 KGD6 R31 123.9 CSU2 KSU31 CGD2 KGD6 R32 123.9 DSU2 KSU32 DGD2 KGD6 R33 123.9 CSU1 KSU33 CGD1 KGD6 R34 123.9 DSU1 KSU34 DGD1 KGD11 R35 123.9 ASU1 KSU35 AGD1 KGD6 CM01 CMD1 KSU2

CM02 CMD2 OMNRL TM01 TLM1 TLML TM02 TLM2 TLML TM03 TLM3 OMNTL R36 123.9 BSU1 KSU36 BGD1 KGD6 F36 125 BGU1 KGU6 BSD1 KSD36 CM04 CMD4 OMNRR OMNTR TM04 TLM4 OMNTR

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 27M0G7W 27000 8 53777 0.7967 10.4 22.4 D2 27M0G7W 27000 8 51523 0.7633 8.5 20.5 D3 27M0G7W 27000 8 47250 0.7 7.9 19.9 D4 27M0G7W 27000 8 46103 0.683 7.4 19.4 D5 27M0G7W 27000 8 42977 0.6367 6.5 18.5 D6 27M0G7W 27000 4 37350 0.83 6.2 18.2 D7 27M0G7W 27000 4 35550 0.79 5.8 17.8 D8 27M0G7W 27000 4 29700 0.66 5.3 17.3 D9 27M0G7W 27000 4 28350 0.63 4.8 16.8 D10 27M0G7W 27000 4 21150 0.47 4.2 16.2 D11 18M0G7W 18000 8 43022 0.7967 9.4 21.4 D12 18M0G7W 18000 8 41218 0.7633 7.5 19.5 D13 18M0G7W 18000 8 37800 0.7 6.9 18.9 D14 18M0G7W 18000 8 36882 0.683 6.4 18.4 D15 18M0G7W 18000 8 34382 0.6367 5.5 17.5 D16 18M0G7W 18000 4 29880 0.83 5.2 17.2 D17 18M0G7W 18000 4 28440 0.79 4.8 16.8 D18 18M0G7W 18000 4 23760 0.66 4.3 16.3 D19 18M0G7W 18000 4 22680 0.63 3.8 15.8 D20 18M0G7W 18000 4 16920 0.47 3.2 15.2 D21 3M20G7W 3200 4 2520 0.492 6.5 19 D22 1M60G2W 1600 4 1260 0.492 6.5 19 D23 800KG7W 800 4 630 0.492 6.5 19 D24 400KG7W 400 4 315 0.492 6.5 19 D25 200KG7W 200 4 157 0.492 6.5 19

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) CMD1 1M00F2D 1000 1 9 21.2 CMD2 1M00F2D 1000 1 9 21.2 TLM1 200KF2D 200 1 9 21.2 TLM2 200KF2D 200 1 9 21.2

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) F1 F36 D1 2 28500 TBS link.doc 65.4 -0.43 8.6 52.6 58.6 -118 16.8 F1 F36 D3 2 28500 TBS link.doc 65.4 -0.43 8.6 49.4 58.6 -118 16.8 F1 F36 D2 2 28500 TBS link.doc 65.4 -0.43 8.6 31.8 58.6 -118 16.8 F1 F36 D4 2 28500 TBS link.doc 65.4 -0.43 8.6 34.8 58.6 -118 16.8 CM01 CM01 CMD1 1 CMD1 LB.doc 65.4 -15.7 -11.7 CM02 CM02 CMD2 1 CMD2 LB.doc 52.3 21.1 25.1 TM01 TM02 TLM1 1 TLM1 LB.doc 13 17.5 -144.5 34.5 TM03 TM03 TLM2 1 TLM2 LB.doc 7.6 9.5 -153 25.6 F1 F36 D5 2 28500 TBS link.doc 65.4 -0.43 8.6 52.6 58.6 -118 16.8 F1 F36 D6 2 28500 F1.doc 65.4 -0.43 8.6 52.6 58.6 -118 16.8 F1 F36 D7 2 28500 TBS link.doc 65.4 -0.43 8.6 52.6 58.6 -118 16.8 F1 F36 D8 2 28500 TBS link.doc 65.4 -0.43 8.6 52.6 58.6 -118 16.8 F1 F36 D9 2 28500 TBS link.doc 65.4 -0.43 8.6 52.6 58.6 -118 16.8 F1 F36 D10 2 28500 TBS link.doc 65.4 -0.43 8.6 52.6 58.6 -118 16.8 F1 F36 D11 3 19000 TBS link.doc 65.4 -1.93 10.3 52.6 58.6 -118 16.8 F1 F36 D12 3 19000 TBS link.doc 65.4 -1.93 10.3 52.6 58.6 -118 16.8 F1 F36 D13 3 19000 TBS link.doc 65.4 -1.93 10.3 52.6 58.6 -118 16.8 F1 F36 D14 3 19000 TBS link.doc 65.4 -1.93 10.3 52.6 58.6 -118 16.8 F1 F36 D15 3 19000 TBS link.doc 65.4 -1.93 10.3 52.6 58.6 -118 16.8 F1 F36 D16 3 19000 TBS link.doc 65.4 -1.93 10.3 52.6 58.6 -118 16.8 F1 F36 D17 3 19000 TBS link.doc 65.4 -1.93 10.3 52.6 58.6 -118 16.8 F1 F36 D18 3 19000 TBS link.doc 65.4 -1.93 10.3 52.6 58.6 -118 16.8 F1 F36 D20 3 19000 TBS link.doc 65.4 -1.93 10.3 52.6 58.6 -118 16.8 R1 R36 D21 132 3200 TBS link.doc 44 -3.5 2.8 53.3 57.3 -118 36.9 R1 R36 D22 264 1600 TBS link.doc 44 -3.5 2.8 53.3 57.3 -118 36.9 R1 R36 D23 528 800 R800.doc 44 -3.5 2.8 53.3 57.3 -118 36.9 R1 R36 D24 1056 400 R400.doc 44 -3.5 2.8 53.3 57.3 -118 36.9 R1 R36 D25 2112 200 TBS link.doc 44 -3.5 2.8 53.3 57.3 -118 36.9

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

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 2100 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2526 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4626 32 0.9 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 666 2.6 0.9 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 60 5.6 0.84 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): 5373 5373 5373 5373 Bus (Watts): (b): (g): (l): (q): 2134 1276 2134 1276 Total (Watts): (c): (h): (m): (r): 7507 6649 7507 6649 Solar Array (Watts): (d): (i): (n): (s): 9648 8658 8178 7478 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? YES NO X 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: 2006-08-14 13:32:21
Document Modified: 2006-08-14 13:32:21
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