Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20050210-00031 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2005021000031_417876

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: IA KAEXT 97W N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 13 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 44 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: 1536 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) 24.75 G 25.25 G R Broadcasting Satellite Service - Video 17.3 G 17.8 G T Broadcasting Satellite Service - Video 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: 97 W Intelsat has license at this location to operate in the C Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be and Ku bands. Adding the extended Ka band will result N/S Station-Keeping provided (Optional): in a more efficient use of the orbital / spectrum d. Toward West: Degrees E/W 0.05 Degrees Tolerance: resources. g. Westernmost: 121 W e. Toward East: 0.05 Degrees 0.05 Degrees h. Easternmost: 67 W i. Reason for service are selection (Optional): The satellite satellite can replace any of the INTELSAT KAEXT spacecrafts located within this arc in case of a catas trophic failure.

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 Service_1_NA.gxt USA, CAN, DOM, HTI, MEX, VIR, PTR, CUB 2 S Service_2_SA.gxt CLM, EQA, PRU, BOL, CHL, PRG, ARG, URG, B, VEN, GUY, SUR 3 S Service_3_US.gxt USA 4 S Service_4_R2.gxt Region 2

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) NTF T 34.5 26 0.15 0.4 30 N 01 3.5 520 58.2 NRF R 35.4 25 0.15 0.4 30 N 0 1 815 6.3 -100 25 1 STF T 31.9 26.2 0.15 0.4 30 N 0 2 3.5 520 55.6 SRF R 35.5 26.2 0.15 0.4 30 N 0 2 815 6.4 -100 25 1 UT1 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT2 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT3 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT4 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT5 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT6 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT7 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 OR R 20.2 17.7 0.15 0.4 30 N 0 4 741 -8.5 -89 25 1 OT T 20 17.5 0.15 0.4 30 N 0 4 2 1 18 GR6 R 46.1 42 0.075 0.4 30 N 0 3 865 16.7 -100 25 1 UT21 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT8 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT9 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT10 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT11 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT12 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT13 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT14 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT15 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT16 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT17 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT18 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT19 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT20 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7 UT22 T 46.1 42 0.075 0.4 30 N 0 3 2.5 130 64.7

UT23 T 46.1 42 0.075 0.4 30 N 03 2.5 130 64.7 GR1 R 46.1 42 0.075 0.4 30 N 0 3 865 16.7 -100 25 1 GR2 R 46.1 42 0.075 0.4 30 N 0 3 865 16.7 -100 25 1 GR3 R 46.1 42 0.075 0.4 30 N 0 3 865 16.7 -100 25 1 GR4 R 46.1 42 0.075 0.4 30 N 0 3 865 16.7 -100 25 1 GR5 R 46.1 42 0.075 0.4 30 N 0 3 865 16.7 -100 25 1 UT24 T 46.1 42 0.075 0.4 30 N 03 2.5 130 64.7

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) NTF T C -97 NTF_X.gxt -128.4 -128.2 -121.7 -121.7 -121.7 STF T C -97 STF_C.gxt -130.2 -127.4 -121.4 -121.4 -121.4 UT1 T C -97 UT1_C.gxt -115.1 -115.1 -115.1 -115.1 -115.1 NTF T X -97 NTF_X.gxt STF T X -97 STF_X.gxt UT1 T X -97 UT1_X.gxt NRF R C -97 NRF_C.gxt SRF R C -97 SRF_C.gxt GR1 R C -97 GR1_C.gxt NRF R X -97 NRF_X.gxt SRF R X -97 SRF_X.gxt GR1 R X -97 GR1_X.gxt OR R C -97 OR_C.gxt OT T C -97 OT_C.gxt -152 -152 -152 -152 -152 OR R X -97 OR_X.gxt OT T X -97 OT_X.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) NT1 24000 T 17323.5 L C N1 126.6 NR1 NRF NT1 NTF NT2 24000 T 17338.08 R C N2 126.6 NR2 NRF NT2 NTF NT3 24000 T 17352.66 L C N3 126.6 NR3 NRF NT3 NTF NT4 24000 T 17367.24 R C N4 126.6 NR4 NRF NT4 NTF NT5 24000 T 17381.82 L C N5 126.6 NR5 NRF NT5 NTF NT6 24000 T 17396.4 R C N6 126.6 NR6 NRF NT6 NTF NT7 24000 T 17410.98 L C N7 126.6 NR7 NRF NT7 NTF NT8 24000 T 17425.56 R C N8 126.6 NR8 NRF NT8 NTF NT9 24000 T 17440.14 L C N9 126.6 NR9 NRF NT9 NTF NT10 24000 T 17454.72 R C N10 126.6 NR10 NRF NT10 NTF NT11 24000 T 17469.3 L C N11 126.6 NR11 NRF NT11 NTF NT12 24000 T 17483.88 R C N12 126.6 NR12 NRF NT12 NTF NT13 24000 T 17498.46 L C N13 126.6 NR13 NRF NT13 NTF NT14 24000 T 17513.04 R C N14 126.6 NR14 NRF NT14 NTF NT15 24000 T 17527.62 L C N15 126.6 NR15 NRF NT15 NTF NT16 24000 T 17542.2 R C N16 126.6 NR16 NRF NT16 NTF NT17 24000 T 17556.78 L C N17 126.6 NR17 NRF NT17 NTF NT18 24000 T 17571.36 R C N18 126.6 NR18 NRF NT18 NTF NT19 24000 T 17585.94 L C N19 126.6 NR19 NRF NT19 NTF NT20 24000 T 17600.52 R C N20 126.6 NR20 NRF NT20 NTF NT21 24000 T 17615.1 L C N21 126.6 NR21 NRF NT21 NTF NT22 24000 T 17629.68 R C N22 126.6 NR22 NRF NT22 NTF NT23 24000 T 17644.26 L C N23 126.6 NR23 NRF NT23 NTF NT24 24000 T 17658.84 R C N24 126.6 NR24 NRF NT24 NTF NT25 24000 T 17673.42 L C N25 126.6 NR25 NRF NT25 NTF NT26 24000 T 17688 R C N26 126.6 NR26 NRF NT26 NTF NT27 24000 T 17702.58 L C N27 126.6 NR27 NRF NT27 NTF NT28 24000 T 17717.16 R C N28 126.6 NR28 NRF NT28 NTF NT29 24000 T 17731.74 L C N29 126.6 NR29 NRF NT29 NTF NT30 24000 T 17746.32 R C N30 126.6 NR30 NRF NT30 NTF

NT31 24000 T 17760.9 L C N31 126.6 NR31 NRF NT31 NTF NT32 24000 T 17775.48 R C N32 126.6 NR32 NRF NT32 NTF ST18 24000 T 17571.36 R C S18 128.7 SR18 SRF ST18 STF ST20 24000 T 17600.52 R C S20 128.7 SR20 SRF ST20 STF ST22 24000 T 17629.68 R C S22 128.7 SR22 SRF ST22 STF ST24 24000 T 17658.84 R C S24 128.7 SR24 SRF ST24 STF ST26 24000 T 17688 R C S26 128.7 SR26 SRF ST26 STF ST28 24000 T 17717.16 R C S28 128.7 SR28 SRF ST28 STF ST30 24000 T 17746.32 R C S30 128.7 SR30 SRF ST30 STF ST32 24000 T 17775.48 R C S32 128.7 SR32 SRF ST32 STF SR18 24000 R 25021.36 L C SX18 128.7 SR18 SRF NT18 NTF SR20 24000 R 25050.52 L C SX20 128.7 SR20 SRF NT20 NTF SR22 24000 R 25079.68 L C SX22 128.7 SR22 SRF NT22 NTF SR24 24000 R 25108.84 L C SX24 128.7 SR24 SRF NT24 NTF SR26 24000 R 25138 L C SX26 128.7 SR26 SRF NT26 NTF SR28 24000 R 25167.16 L C SX28 128.7 SR28 SRF NT28 NTF SR30 24000 R 25196.32 L C SX30 128.7 SR30 SRF NT30 NTF SR32 24000 R 25225.48 L C SX32 128.7 SR32 SRF NT32 NTF NR1 24000 R 24773.5 R C NX18 126.6 NR18 NRF ST18 STF NR2 24000 R 24788.08 L C NX20 126.6 NR20 NRF ST20 STF NR3 24000 R 24802.66 R C NX22 126.6 NR22 NRF ST22 STF NR4 24000 R 24817.24 L C NX24 126.6 NR24 NRF ST24 STF NR5 24000 R 24831.82 R C NX26 126.6 NR26 NRF ST26 STF NR6 24000 R 24846.4 L C NX28 126.6 NR28 NRF ST28 STF NR7 24000 R 24860.98 R C NX30 126.6 NR30 NRF ST30 STF NR8 24000 R 24875.56 L C NX32 126.6 NR32 NRF ST32 STF NR9 24000 R 24890.14 R C G6A 113.5 G24 GR6 U24 UT6 NR10 24000 R 24904.72 L C G6B 113.5 G68 GR6 U68 UT8 NR11 24000 R 24919.3 R C G6C 113.5 G1012 GR6 U1012 UT9 NR12 24000 R 24933.88 L C G6D 113.5 G1416 GR6 U1416 UT7 NR13 24000 R 24948.46 R C G1A 113.5 G24 GR1 U24 UT1 NR14 24000 R 24963.04 L C G1B 113.5 G68 GR1 U68 UT4 NR15 24000 R 24977.62 R C G1C 113.5 G1012 GR1 U1012 UT24 NR16 24000 R 24992.2 L C G1D 113.5 G1416 GR1 U1416 UT23 NR17 24000 R 25006.78 R C G2A 113.5 G24 GR2 U24 UT10 NR18 24000 R 25021.36 L C G2B 113.5 G68 GR2 U68 UT14 NR19 24000 R 25035.94 R C G2C 113.5 G1012 GR2 U1012 UT13 NR20 24000 R 25050.52 L C G2D 113.5 G1416 GR2 U1416 UT11 NR21 24000 R 25065.1 R C G3A 113.5 G24 GR3 U24 UT15

NR22 24000 R 25079.68 L C G3B 113.5 G68 GR3 U68 UT16 NR23 24000 R 25094.26 R C G3C 113.5 G1012 GR3 U1012 UT12 NR24 24000 R 25108.84 L C G3D 113.5 G1416 GR3 U1416 UT21 NR25 24000 R 25123.42 R C G4A 113.5 G24 GR4 U24 UT17 NR26 24000 R 25138 L C G4B 113.5 G68 GR4 U68 UT18 NR27 24000 R 25152.58 R C G4C 113.5 G1012 GR4 U1012 UT5 NR28 24000 R 25167.16 L C G4D 113.5 G1416 GR4 U1416 UT22 NR29 24000 R 25181.74 R C G5A 113.5 G24 GR5 U24 UT19 NR30 24000 R 25196.32 L C G5B 113.5 G68 GR5 U68 UT20 NR31 24000 R 25210.9 R C G5C 113.5 G1012 GR5 U1012 UT2 NR32 24000 R 25225.48 L C G5D 113.5 G1416 GR5 U1416 UT3 G24 48000 R 24802.66 L C G68 48000 R 24860.98 L C G1012 48000 R 24919.30 L C G1416 48000 R 24977.62 L C U24 48000 T 17352.66 R C U68 48000 T 17410.98 R C U1012 48000 T 14469.30 R C U1416 48000 T 17527.62 R C TLC1 1000 R 5925.5 V T TLC2 1000 R 6424.5 H T TLC3 1000 R 24751.5 R T TLC4 1000 R 25248.5 R T TLM1 1000 T 4197.5 V T TLM2 1000 T 4198.5 V T TLM3 1000 T 17301.5 L T TLM4 1000 T 17303.5 L T TLM5 1000 T 17797.5 R T TLM6 1000 T 17799.5 R T TLC5 1000 R 24753.5 R T TLC6 1000 R 25246.5 R 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) 1 24M0G7W 24000 4 26650 0.6667 4.1 16.3 2 48M0G7W 48000 8 100000 0.8333 8.9 21.1 3 48M0G7W 48000 8 80000 0.6667 9.6 21.8 4 24M0G7W 24000 8 50000 0.8333 8.9 21.1 5 24M0G7W 24000 8 40000 0.6667 9.6 21.8

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) 1 1M00F2D 1000 FM 1 14.3 21 2 50K0N0N 50 1 4 21 3 350KG9D 350 1 13.9 21

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) SX18 SX32 1 1 Link_Budget.do 65.3 7.9 13.4 50 54 -121.7 12.9 SX18 SX32 1 1 Link_Budget.do 65.3 7.9 13.4 50.5 53 -122.5 18.9 SX18 SX32 1 1 Link_Budget.do 65.3 7.9 13.4 50.1 54.1 -121.6 13.1 SX18 SX32 1 1 Link_Budget.do 65.3 7.9 13.4 53.7 56.2 -119.3 16.3 NX18 NX32 1 1 Link_Budget.do 65.1 10.3 12.2 50.9 51.9 -123.8 13.1 NX18 NX32 1 1 Link_Budget.do 65.1 10.3 12.2 52.7 53.9 -122.3 19 NX18 NX32 1 1 Link_Budget.do 65.1 9.2 11.1 50.9 51.9 -123.8 13.1 NX18 NX32 1 1 Link_Budget.do 65.1 9.2 11.1 52.7 53.9 -122.3 19 NX18 NX32 1 1 Link_Budget.do 65.3 7.6 9.5 50.9 51.9 -123.8 13.1 NX18 NX32 1 1 Link_Budget.do 65.3 7.6 9.5 52.7 53.9 -122.3 19 NX18 NX32 1 1 Link_Budget.do 65.3 9.6 11.5 50.9 51.9 -123.8 13.1 NX18 NX32 1 1 Link_Budget.do 65.3 9.6 11.5 52.7 53.9 -122.3 19 N1 N32 1 1 Link_Budget.do 65.1 10.3 12.2 50 54 -121.7 12.9 N1 N32 1 1 Link_Budget.do 65.1 9.2 11.1 50.5 53 -122.5 18.9 N1 N32 1 1 Link_Budget.do 65.3 7.6 9.5 50.1 54.1 -121.6 13.1 N1 N32 1 1 Link_Budget.do 65.3 9.6 11.5 53.7 56.2 -119.3 16.3 S18 S32 1 1 Link_Budget.do 65.3 6 11.5 50.9 51.9 -123.8 13.1 S18 S32 1 1 Link_Budget.do 65.3 7.9 13.4 52.7 53.9 -122.3 19 G1A G6D 2 1 Link_Budget.do 65.1 6.8 11.8 59.4 63.5 -116.1 12.7 G1A G6D 2 1 Link_Budget.do 65.1 6.6 11.6 59.2 63.3 -115.3 12.9 G1A G6D 3 1 Link_Budget.do 65.1 6.8 11.8 59.4 63.5 -116.1 11.4 G1A G6D 3 1 Link_Budget.do 65.1 6.6 11.6 59.2 63.3 -115.3 11.1 G1A G6D 4 2 24000 Link_Budget.do 65.1 4 9 56.6 60.7 -115.9 12.7 G1A G6D 4 2 24000 Link_Budget.do 65.1 3.7 8.7 56.3 60.4 -115.1 12.9 G1A G6D 5 2 24000 Link_Budget.do 65.1 4 9 56.6 60.7 -115.9 11.4 G1A G6D 5 2 24000 Link_Budget.do 65.1 3.7 8.7 56.3 60.4 -115.1 11.1 SX18 SX32 1 1 Link_Budget.do 65.3 6 11.5 50 54 -121.7 12.9 SX18 SX32 1 1 Link_Budget.do 65.3 6 11.5 50.5 53 -122.5 18.9 SX18 SX32 1 1 Link_Budget.do 65.3 6 11.5 50.1 54.1 -121.6 13.1

SX18 SX32 1 1 Link_Budget.do 65.3 6 11.5 53.7 56.2 -119.3 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: 17625 Technology Bld S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Hagerstown Washington MD 21740 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 240-420-8991 Remote Control (TT C) Location(s): S14a: Street Address: 22021 COMSAT Drive S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Clarksburg Montgomery MD 20871 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 301-428-1501

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 3300 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3400 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6700 11 0.83 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1100 3.5 0.87 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 100 7 0.7 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): 14420 14420 14420 14420 Bus (Watts): (b): (g): (l): (q): 3330 2310 3330 2130 Total (Watts): (c): (h): (m): (r): 17750 16550 17750 16550 Solar Array (Watts): (d): (i): (n): (s): 24300 20960 18550 15940 Depth of Battery (e) (j) (o) (t) Discharge (%): 74 % 74 % 74 % 74 % 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: 2005-02-14 08:15:52
Document Modified: 2005-02-14 08:15:52
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC