Attachment Schedule S Tech Data

This document pretains to SAT-RPL-20090123-00007 for Replacement Application on a Satellite Space Stations filing.

IBFS_SATRPL2009012300007_694188

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: IS 14 10/1/2009 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 1/10/2007 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 6/1/2009 62 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: 7/1/2009 9/1/2009 2448 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 14000 M 14500 M R Fixed Satellite Service 11450 M 11950 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: 45 W TO REPLACE THE INTELSAT IR SPACECRAFT Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be CURRENTLY OPERATING AT 45W 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 EUROPE AND AFRICA 2 S AMERICAS 3 S EUROPE, AFRICA, USA 4 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) CEU R 30.6 20.6 0.39 0.12 N 01 519 3.5 -102.8 21 1 CEU R 30.6 20.6 0.39 0.12 N 90 1 519 3.5 -102.8 21 1 CEU R 32.2 22.2 0.39 0.12 N 1 594 4.5 -104.4 21 1 CEU R 32.2 22.2 0.39 0.12 N 1 594 4.5 -104.4 21 1 CAU R 28.1 18.1 0.39 0.12 Y 02 563 0.6 -100.1 21 1 CAU R 28.1 18.1 0.39 0.12 Y 90 2 563 0.6 -100.1 21 1 KEU R 35.3 25.3 0.39 0.12 N 0 3 592 7.6 -103 21 1 KEU R 35.3 25.3 0.39 0.12 N 90 3 592 7.6 -103 21 1 KAU R 30.8 22.8 0.39 0.12 N 0 2 634 2.8 -101.2 21 1 KAU R 30.8 22.8 0.39 0.12 N 90 2 634 2.8 -101.2 21 1 CED T 30.2 22.2 0.39 0.12 N 01 2.1 30.9 45.1 CED T 30.2 22.2 0.39 0.12 N 90 1 2.1 30.9 45.1 CED T 29.9 19.9 0.39 0.12 N 1 2.5 33.9 45.2 CED T 29.9 19.9 0.39 0.12 N 1 2.5 33.9 45.2 CAD T 27.2 17.2 0.39 0.12 N 02 2.1 39.8 43.3 CAD T 27.4 17.4 0.39 0.12 N 90 2 2.1 39.8 43.5 KED T 33.9 25.9 0.39 0.12 N 0 3 1.8 100 53.9 KED T 33.9 25.9 0.39 0.12 N 90 3 1.8 100 53.9 KAD T 29.7 23.7 0.39 0.12 N 0 2 2.1 93.3 49.4 KAD T 29.6 23.6 0.39 0.12 N 90 2 2.1 93.3 49.3 CMD R 28.1 20.8 0.39 0.12 N 90 2 32310 -16.9 -117.8 CMD R 2 -4 0.39 0.12 N 4 5129 -35.1 -99.5 CMD R 6 0 0.39 0.12 N 4 30803 -38.9 -95.9 TLM T 27.2 21.1 0.39 0.12 N 02 6 0.1 17.2 TLM T 2 -4 0.39 0.12 N 4 4.5 15.8 14 TLM T 6 0 0.39 0.12 N 4 11.1 3.5 11.4 UPC T 22.3 19.7 0.39 0.12 N 04 3.7 0.2 14.6 UPC T 22.3 19.7 0.39 0.12 N 90 4 3.7 0.2 14.6 UPK T 22.2 19.6 0.39 0.12 N 04 5.7 0.3 16.5

UPK T 22.2 19.6 0.39 0.12 N 90 4 5.7 0.3 16.5

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) CEU R C -45 ceuh.gxt CEU R C -45 ceuv.gxt CEU R C -45 ceur.gxt CEU R C -45 ceul.gxt CAU R C -45 cauh.gxt CAU R C -45 cauv.gxt KEU R C -45 keuh.gxt KEU R C -45 keuv.gxt KAU R C -45 kauh.gxt KAU R C -45 kauv.gxt CED T C -45 cedh.gxt -152 -149.5 -147.9 -147.8 -147.7 CED T C -45 cedv.gxt -152 -149.5 -147.9 -147.8 -147.7 CED T C -45 cedr.gxt -152 -149.5 -147.8 -147.7 -147.6 CED T C -45 cedl.gxt -152 -149.5 -147.8 -147.7 -147.6 CAD T C -45 cadh.gxt -152 -149.9 -149.7 -149.6 -149.5 CAD T C -45 cadv.gxt -152 -149.7 -149.5 -149.4 -149.3 KED T C -45 kedh.gxt -150 -147.5 -145 -142.5 -140 KED T C -45 kedv.gxt -150 -147.5 -145 -142.5 -140 KAD T C -45 kadh.gxt KAD T C -45 kadv.gxt CMD R C -45 cmdc.gxt CMD R C -45 CMDW.pdf CMD R C -45 CMDM.pdf TLM T C -45 tlmc.gxt -166.6 -166.5 -166.4 -166.2 -166.1 TLM T C -45 TLMW.pdf -169.8 -169.7 -169.6 -169.4 -169.3 TLM T C -45 TLMM.pdf -172.4 -172.3 -172.2 -172 -171.9 UPC T C -45 upch.gxt -156.6 -156.5 -156.4 -156.3 -156.2 UPC T C -45 upcv.gxt -156.6 -156.5 -156.4 -156.3 -156.2

UPK T C -45 upkh.gxt -154.7 -154.6 -154.5 -154.4 -154.3 UPK T C -45 upkv.gxt -154.7 -154.6 -154.5 -154.4 -154.3 CEU R X S8_SCHEDULE_S_NOTE.pdf -45 CEU R X S8_SCHEDULE_S_NOTE.pdf -45 CEU R X S8_SCHEDULE_S_NOTE.pdf -45 CEU R X S8_SCHEDULE_S_NOTE.pdf -45 CAU R X S8_SCHEDULE_S_NOTE.pdf -45 CAU R X S8_SCHEDULE_S_NOTE.pdf -45 KEU R X S8_SCHEDULE_S_NOTE.pdf -45 KEU R X S8_SCHEDULE_S_NOTE.pdf -45 KAU R X S8_SCHEDULE_S_NOTE.pdf -45 KAU R X S8_SCHEDULE_S_NOTE.pdf -45 CED T X S8_SCHEDULE_S_NOTE.pdf -45 CED T X S8_SCHEDULE_S_NOTE.pdf -45 CED T X S8_SCHEDULE_S_NOTE.pdf -45 CED T X S8_SCHEDULE_S_NOTE.pdf -45 CAD T X S8_SCHEDULE_S_NOTE.pdf -45 CAD T X S8_SCHEDULE_S_NOTE.pdf -45 KED T X S8_SCHEDULE_S_NOTE.pdf -45 KED T X S8_SCHEDULE_S_NOTE.pdf -45 KAD T X S8_SCHEDULE_S_NOTE.pdf -45 KAD T X S8_SCHEDULE_S_NOTE.pdf -45

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) 1CU 36000 R 5960 V C 1C 124.2 1CU CEUV 1CD CEDH 3CU 36000 R 6000 V C 3C 124.2 3CU CEUV 3CD CEDH 5CU 36000 R 6040 V C 5C 124.2 5CU CEUV 5CD CEDH 7CU 36000 R 6080 V C 7C 124.2 7CU CEUV 7CD CEDH 9CU 36000 R 6120 V C 9C 124.2 9CU CEUV 9CD CEDH 11CU 36000 R 6160 V C 11C 124.2 11CU CEUV 11CD CEDH 13CU 36000 R 6200 L C 13C 124.9 13CU CEUL 13CD CEDR 15CU 36000 R 6240 L C 15C 124.9 15CU CEUL 15CD CEDR 17CU 36000 R 6280 L C 17C 124.9 17CU CEUL 17CD CEDR 19CU 36000 R 6320 L C 19C 124.9 19CU CEUL 19CD CEDR 21CU 36000 R 6360 L C 21C 124.9 21CU CEUL 21CD CEDR 23CU 36000 R 6400 L C 23C 124.9 23CU CEUL 23CD CEDR 2CU 36000 R 5960 H C 2C 124.2 2CU CEUH 2CD CEDV 4CU 36000 R 6000 H C 4C 124.2 4CU CEUH 4CD CEDV 6CU 36000 R 6040 H C 6C 124.2 6CU CEUH 6CD CEDV 8CU 36000 R 6080 H C 8C 124.2 8CU CEUH 8CD CEDV 10CU 36000 R 6120 H C 10C 124.2 10CU CEUH 10CD CEDV 12CU 36000 R 6160 H C 12C 124.2 12CU CEUH 12CD CEDV 14CU 36000 R 6200 R C 14C 124.9 14CU CEUR 14CD CEDL 16CU 36000 R 6240 R C 16C 124.9 16CU CEUR 16CD CEDL 18CU 36000 R 6280 R C 18C 124.9 18CU CEUR 18CD CEDL 20CU 36000 R 6320 R C 20C 124.9 20CU CEUR 20CD CEDL 22CU 36000 R 6360 R C 22C 124.9 22CU CEUR 22CD CEDL 24CU 36000 R 6400 R C 24C 124.9 24CU CEUR 24CD CEDL 25CU 36000 R 5960 V C 25C 125.4 25CU CAUV 25CD CADH 27CU 36000 R 6000 V C 27C 125.4 27CU CAUV 27CD CADH 29CU 36000 R 6040 V C 29C 125.4 29CU CAUV 29CD CADH 31CU 36000 R 6080 V C 31C 125.4 31CU CAUV 31CD CADH 33CU 72000 R 6142 V C 33C 125.4 33CU CAUV 33CD CADH 35CU 72000 R 6222 V C 35C 125.4 35CU CAUV 35CD CADH

37CU 72000 R 6302 V C 37C 125.4 37CU CAUV 37CD CADH 39CU 72000 R 6382 V C 39C 125.4 39CU CAUV 39CD CADH 26CU 36000 R 5960 H C 26C 125.4 26CU CAUH 26CD CADV 28CU 36000 R 6000 H C 28C 125.4 28CU CAUH 28CD CADV 30CU 36000 R 6040 H C 30C 125.4 30CU CAUH 30CD CADV 32CU 36000 R 6080 H C 32C 125.4 32CU CAUH 32CD CADV 34CU 72000 R 6142 H C 34C 125.4 34CU CAUH 34CD CADV 36CU 72000 R 6222 H C 36C 125.4 36CU CAUH 36CD CADV 38CU 72000 R 6302 H C 38C 125.4 38CU CAUH 38CD CADV 40CU 72000 R 6382 H C 40C 125.4 40CU CAUH 40CD CADV 25HU 36000 R 5960 H C 25H 125.4 25HU CAUH 25CD CADH 27HU 36000 R 6000 H C 27H 125.4 27HU CAUH 27CD CADH 29HU 36000 R 6040 H C 29H 125.4 29HU CAUH 29CD CADH 31HU 36000 R 6080 H C 31H 125.4 31HU CAUH 31CD CADH 33HU 72000 R 6142 H C 33H 125.4 33HU CAUH 33CD CADH 35HU 72000 R 6222 H C 35H 125.4 35HU CAUH 35CD CADH 37HU 72000 R 6302 H C 37H 125.4 37HU CAUH 37CD CADH 39HU 72000 R 6382 H C 39H 125.4 39HU CAUH 39CD CADH 26VU 36000 R 5960 V C 26V 125.4 26VU CAUV 26CD CADV 28VU 36000 R 6000 V C 28V 125.4 28VU CAUV 28CD CADV 30VU 36000 R 6040 V C 30V 125.4 30VU CAUV 30CD CADV 32VU 36000 R 6080 V C 32V 125.4 32VU CAUV 32CD CADV 34VU 72000 R 6142 V C 34V 125.4 34VU CAUV 34CD CADV 36VU 72000 R 6222 V C 36V 125.4 36VU CAUV 36CD CADV 38VU 72000 R 6302 V C 38V 125.4 38VU CAUV 38CD CADV 40VU 72000 R 6382 V C 40V 125.4 40VU CAUV 40CD CADV 1KU 36000 R 14020 V C 1K 132.1 1KU KEUV 1KD KEDH 3KU 36000 R 14060 V C 3K 132.1 3KU KEUV 3KD KEDH 5KU 36000 R 14100 V C 5K 132.1 5KU KEUV 5KD KEDH 7KU 36000 R 14140 V C 7K 132.1 7KU KEUV 7KD KEDH 9KU 72000 R 14202 V C 9K 132.1 9KU KEUV 9KD KEDH 11KU 36000 R 14270 V C 11K 132 11KU KAUV 11KD KADH 13KU 36000 R 14310 V C 13K 132 13KU KAUV 13KD KADH 15KU 36000 R 14350 V C 15K 132 15KU KAUV 15KD KADH 17KU 36000 R 14390 V C 17K 132 17KU KAUV 17KD KADH 19KU 36000 R 14430 V C 19K 132 19KU KAUV 19KD KADH 21KU 36000 R 14470 V C 21K 132 21KU KAUV 21KD KADH 2KU 36000 R 14020 H C 2K 132.1 2KU KEUH 2KD KEDV 4KU 36000 R 14060 H C 4K 132.1 4KU KEUH 4KD KEDV

6KU 36000 R 14100 H C 6K 132.1 6KU KEUH 6KD KEDV 8KU 36000 R 14140 H C 8K 132.1 8KU KEUH 8KD KEDV 10KU 72000 R 14202 H C 10K 132.1 10KU KEUH 10KD KEDV 12KU 36000 R 14270 H C 12K 132 12KU KAUH 12KD KADV 14KU 36000 R 14310 H C 14K 132 14KU KAUH 14KD KADV 16KU 36000 R 14350 H C 16K 132 16KU KAUH 16KD KADV 18KU 36000 R 14390 H C 18K 132 18KU KAUH 18KD KADV 20KU 36000 R 14430 H C 20K 132 20KU KAUH 20KD KADV 22KU 36000 R 14470 H C 22K 132 22KU KAUH 22KD KADV 1CD 36000 T 3735 H C 3CD 36000 T 3775 H C 5CD 36000 T 3815 H C 7CD 36000 T 3855 H C 9CD 36000 T 3895 H C 11CD 36000 T 3935 H C 13CD 36000 T 3975 R C 15CD 36000 T 4015 R C 17CD 36000 T 4055 R C 19CD 36000 T 4095 R C 21CD 36000 T 4135 R C 23CD 36000 T 4175 R C 2CD 36000 T 3735 V C 4CD 36000 T 3775 V C 6CD 36000 T 3815 V C 8CD 36000 T 3855 V C 10CD 36000 T 3895 V C 12CD 36000 T 3935 V C 14CD 36000 T 3975 L C 16CD 36000 T 4015 L C 18CD 36000 T 4055 L C 20CD 36000 T 4095 L C 22CD 36000 T 4135 L C 24CD 36000 T 4175 L C 25CD 36000 T 3735 H C 27CD 36000 T 3775 H C 29CD 36000 T 3815 H C 31CD 36000 T 3855 H C 33CD 72000 T 3917 H C 35CD 72000 T 3997 H C

37CD 72000 T 4077 H C 39CD 72000 T 4157 H C 26CD 36000 T 3735 V C 28CD 36000 T 3775 V C 30CD 36000 T 3815 V C 32CD 36000 T 3855 V C 34CD 72000 T 3917 V C 36CD 72000 T 3997 V C 38CD 72000 T 4077 V C 40CD 72000 T 4157 V C 25CD 36000 T 3735 H C 27CD 36000 T 3775 H C 29CD 36000 T 3815 H C 31CD 36000 T 3855 H C 33CD 72000 T 3917 H C 35CD 72000 T 3997 H C 37CD 72000 T 4077 H C 39CD 72000 T 4157 H C 26CD 36000 T 3735 V C 28CD 36000 T 3775 V C 30CD 36000 T 3815 V C 32CD 36000 T 3855 V C 34CD 72000 T 3917 V C 36CD 72000 T 3997 V C 38CD 72000 T 4077 V C 40CD 72000 T 4157 V C 1KD 36000 T 11470 H C 3KD 36000 T 11510 H C 5KD 36000 T 11550 H C 7KD 36000 T 11590 H C 9KD 72000 T 11652 H C 11KD 36000 T 11720 H C 13KD 36000 T 11760 H C 15KD 36000 T 11800 H C 17KD 36000 T 11840 H C 19KD 36000 T 11880 H C 21KD 36000 T 11920 H C 2KD 36000 T 11470 V C 4KD 36000 T 11510 V C

6KD 36000 T 11550 V C 8KD 36000 T 11590 V C 10KD 72000 T 11652 V C 12KD 36000 T 11720 V C 14KD 36000 T 11760 V C 16KD 36000 T 11800 V C 18KD 36000 T 11840 V C 20KD 36000 T 11880 V C 22KD 36000 T 11920 V C CMD1 1000 R 5927 V T CMD2 1000 R 5932 V T CMD3 1000 R 5927 L T CMD4 1000 R 5932 L T TLM1 500 T 3709 H T TLM2 500 T 3710 H T TLM3 500 T 3709 R T TLM4 500 T 3710 R T UPC1 25 T 3704 H T UPC2 25 T 3705 V T UPC3 25 T 11695 H T UPC4 25 T 11694 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 72M0G7W 72000 4 55539.3 0.5 3.4 10.1 D2 36M0G7W 36000 4 27769.6 0.5 3.4 10.3 D3 10M3G7W 6771 4 10300 0.5 3.9 11 D4 1M45G7W 1450 2 614.5 0.5 3.4 9.5 D5 400KG7W 400 2 153.5 0.5 3.4 10.7 D6 100KG7W 100 4 70.4 0.5 3 9.6

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 36M0F3F 36000 TV/FM 1 PAL 15.6 1.5 10 18.8

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 40C A1 1 Link_Budgets.p 4000 49.7 13.5 23.5 28.3 36.3 -155.8 21.4 1C 40C D2 1 S13_SCHEDUL 49.7 13.3 23.3 37.1 45.1 -155.8 18.8 1C 40C D3 3 10300 S13_SCHEDUL 49.7 4.8 14.8 30.6 38.6 -155.8 19.6 1C 40C D6 360 100 S13_SCHEDUL 49.7 -14.7 -4.7 11.1 19.1 -155.8 19 1C 40C A1 1 S13_SCHEDUL 4000 50.1 13.5 23.5 26.4 36.4 -155.7 22.7 1C 40C D2 1 S13_SCHEDUL 50.1 13.3 23.3 35.2 45.2 -155.7 19 1C 40C D3 3 10300 S13_SCHEDUL 50.1 4.8 14.8 28.7 38.7 -155.7 19.8 1C 40C D6 360 100 S13_SCHEDUL 50.1 -14.7 -4.7 9.2 19.2 -155.7 19.2 1C 40C A1 1 S13_SCHEDUL 4000 49.7 13.9 23.9 24.5 34.5 -157.6 23.5 1C 40C D2 1 S13_SCHEDUL 49.7 13.7 23.7 33.3 43.3 -157.6 19.2 1C 40C D3 3 10300 S13_SCHEDUL 49.7 5.2 15.2 26.8 36.8 -157.6 20.1 1C 40C D6 360 100 S13_SCHEDUL 49.7 -14.3 -4.3 7.3 17.3 -157.6 19.5 1C 40C A1 2 36000 S13_SCHEDUL 4000 50 13.6 23.6 21.5 31.5 -160.6 26.3 1C 40C D1 1 S13_SCHEDUL 50 13.4 23.4 33.3 43.3 -160.6 20.8 1C 40C D3 6 10300 S13_SCHEDUL 50 1.9 11.9 23.8 33.8 -160.6 25.3 1C 40C D6 720 100 S13_SCHEDUL 50 -17.6 -7.6 4.3 14.3 -160.6 21.9 1K 22K A1 1 S13_SCHEDUL 4000 57.1 11.8 21.8 39 47 -145.1 21.1 1K 22K D2 1 S13_SCHEDUL 57.1 -6.4 3.6 40.8 48.8 -152.1 21.1 1K 22K D3 3 S13_SCHEDUL 57.1 7.1 17.1 34.3 42.3 -152.1 21.5 1K 22K D6 360 S13_SCHEDUL 57.1 -12.4 -2.4 14.8 22.8 -152.1 20.7 1K 22K D4 24 S13_SCHEDUL 57.1 -0.5 9.5 26.7 34.7 -152.3 20.8 1K 22K D5 90 S13_SCHEDUL 44.5 -6 4 8.6 16.6 -164.4 26.4 1K 22K A1 2 S13_SCHEDUL 4000 57.1 8.8 18.8 39 47 -145.1 21.3 1K 22K D1 1 S13_SCHEDUL 57.1 13.6 23.6 43.8 51.8 -152.1 21.3 1K 22K D2 2 S13_SCHEDUL 57.1 10.6 20.6 40.8 48.8 -152.1 21.5 1K 22K D3 6 S13_SCHEDUL 57.1 4.1 14.1 34.3 42.3 -152.1 21.7 1K 22K D6 720 S13_SCHEDUL 57.1 -15.4 -5.4 14.8 22.8 -152.1 20.9 1K 22K D4 49 S13_SCHEDUL 57.1 -3.4 6.6 26.8 34.8 -152.2 20.9 1K 22K D5 180 S13_SCHEDUL 44.5 -9.3 0.7 9.3 17.3 -163.7 -2.4

1K 22K A1 1 S13_SCHEDUL 4000 57.2 13.8 21.8 41 47 -145.1 19.6 1K 22K D2 1 S13_SCHEDUL 57.2 15.6 23.6 42.8 48.8 -152.1 19.6 1K 22K D3 3 S13_SCHEDUL 57.2 9.1 17.1 36.3 42.3 -152.1 19.9 1K 22K D6 360 S13_SCHEDUL 57.2 -10.4 -2.4 16.8 22.8 -152.1 19.4 1K 22K D4 24 S13_SCHEDUL 57.2 1.7 9.7 28.9 34.9 -152.1 19.4 1K 22K D5 90 S13_SCHEDUL 43.1 -4.1 3.9 9 15 -166 33.5

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: 3400 INTERNATIONAL DRIVE S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: WASHINGTON DC 20008 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 202-944-7701

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 2517 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3146 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5663 26.1 0.862 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 967 7.7 0.763 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 74.3 14 0.658 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): 10071 10071 10071 10071 Bus (Watts): (b): (g): (l): (q): 2648 1233 2648 1233 Total (Watts): (c): (h): (m): (r): 12719 11304 12719 11304 Solar Array (Watts): (d): (i): (n): (s): 15000 13335 13404 11916 Depth of Battery (e) (j) (o) (t) Discharge (%): 66.8 % % 70.8 % % 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: 2009-02-03 16:34:07
Document Modified: 2009-02-03 16:34:07
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC