Attachment Sched S Tech Report

This document pretains to SAT-LOA-20101014-00219 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2010101400219_845607

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: INTELSAT 18 4/30/2011 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 8/4/2008 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 2/17/2011 36 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: 3/1/2011 3/31/2011 2170 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 14000 M 14500 M R Fixed Satellite Service 3700 M 4200 M T Fixed Satellite Service 10950 M 11200 M T Fixed Satellite Service 11450 M 11700 M T Fixed Satellite Service 12250 M 12750 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: 180 E REPLACE THE EXISTING INTELSAT 701 Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be SPACECRAFT 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 EAST ASIA, WESTERN NORTH AMERICA, NORTHERN PACIFIC 2 S AUSTRALIA, NEW ZEALAND, SOUTHERN PACIFIC 3 S SOUTHEAST PACIFIC, WESTERN NORTH AMERICA 4 S EASTERN AUSTRALIA, NEW ZEALAND, SOUTHWESTERN PACIFIC 5 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) NAL R 29.3 23.3 0.1 0.1 30 N 1 457 2.7 -108.1 32 1 NBR R 29.3 23.3 0.1 0.1 30 N 1 457 2.7 -108.1 32 1 SALU R 26.8 20.8 0.1 0.1 20 N 2 468 0.1 -105.6 32 1 SBR R 26.8 20.8 0.1 0.1 20 N 2 468 0.1 -105.6 32 1 GAL R 20.8 16.8 0.1 0.1 30 N 5 427 -5.5 -99.3 32 1 GBR R 20.8 16.8 0.1 0.1 30 N 5 427 -5.5 -99.3 32 1 F1HU R 36.2 30.2 0.1 0.1 30 N 0 3 631 8.2 -107.7 32 1 F2HU R 34.9 28.9 0.1 0.1 30 N 0 4 631 6.9 -106.3 32 1 F2VU R 34.8 28.8 0.1 0.1 30 N 90 4 631 6.8 -106.4 32 1 USV R 36.3 30.3 0.1 0.1 30 N 90 3 631 8.3 -107.8 32 1 NAR T 27.6 21.6 0.1 0.1 30 N 1 2.6 24.5 41.5 NBL T 27.7 21.7 0.1 0.1 30 N 1 2.6 24.5 41.6 SAR T 26.5 20.5 0.1 0.1 30 N 2 2.6 24.5 40.4 SBLD T 26.5 20.5 0.1 0.1 20 N 2 2.6 24.5 40.4 GAR T 20.4 16.4 0.1 0.1 30 N 5 2 28.2 34.9 GBL T 20.4 16.4 0.1 0.1 30 N 5 2 28.2 34.9 F1VD T 34.5 28.5 0.1 0.1 30 N 90 3 3 75.9 53.3 F2VD T 34 28 0.1 0.1 30 N 90 4 3 75.9 52.8 F2HD T 33.8 27.8 0.1 0.1 30 N 04 3 75.9 52.6 CMD R 20.8 16.8 0.1 0.1 N 5 9371 -18.9 -115.3 CMD R 13.1 9.1 0.1 0.1 N 5 22510 -30.4 -103.9 CMD R 2.4 -1.6 0.1 0.1 N 5 7613 -36.4 -97.8 TLM T 20.4 16.4 0.1 0.1 N 5 5.2 0.2 12.8 TLM T 13.1 9.1 0.1 0.1 N 5 10 1 13.1 TLM T 1.8 -2.2 0.1 0.1 N 5 5.3 2.9 6.5 UPC T 13 9 0.1 0.1 N 90 5 2.8 0.5 10 UPC T 20.6 16.6 0.1 0.1 N 5 5.4 0.18 13.2

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) NAL R C 180 NALU.gxt NBR R C 180 NBRU.gxt SALU R C 180 SALU.gxt SBR R C 180 SBRU.gxt GAL R C 180 GALU.gxt GBR R C 180 GBRU.gxt F1HU R C 180 F1HU.gxt F2HU R C 180 F2HU.gxt F2VU R C 180 F2VU.gxt USV R C 180 USVU.gxt NAR T C 180 NARD.gxt -152 -151.7 -151.5 -151.4 -151.3 NBL T C 180 NBLD.gxt -152 -151.6 -151.4 -151.3 -151.2 SAR T C 180 SARD.gxt -152.9 -152.8 -152.6 -152.5 -152.4 SBLD T C 180 SBLD.gxt -152.9 -152.8 -152.6 -152.5 -152.4 GAR T C 180 GARD.gxt -158.4 -158.3 -158.1 -158 -157.9 GBL T C 180 GBLD.gxt -158.4 -158.3 -158.1 -158 -157.9 F1VD T C 180 F1VD.gxt -150 -147.5 -145 -142.5 -140 F2VD T C 180 F2VD.gxt -148 -145.5 -143 -140.5 -140 F2HD T C 180 F2HD.gxt -148 -145.5 -143 -140.5 -140.2 CMD R C 180 CMDG.gxt CMD R C 180 CMDW.pdf CMD R C 180 CMDO.pdf TLM T C 180 TLMG.gxt -168.4 -168.3 -168.2 -168.1 -168 TLM T C 180 TLMW.pdf -168.1 -168 -167.9 -167.8 -167.7 TLM T C 180 TLMO.pdf -174.7 -174.6 -174.5 -174.4 -174.3 UPC T C 180 UPCC.pdf -161.2 -161.1 -161 -160.9 -160.8 UPC T C 180 UPCK.pdf -158 -157.9 -157.8 -157.7 -157.6

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 72000 R 5970 L C C0001 129.9 1CU NALU 1CD NARD 3CU 72000 R 6050 L C C0003 129.9 3CU NALU 3CD NARD 5CU 72000 R 6130 L C C0005 129.9 5CU NALU 5CD NARD 7CU 72000 R 6220 L C C0007 129.9 7CU NALU 7CD NARD 9CU 72000 R 5970 L C CX001 129.9 1CU NALU 9CD SARD 11CU 72000 R 6050 L C CX003 129.9 3CU NALU 11CD SARD 13CU 72000 R 6130 L C CX005 129.9 5CU NALU 13CD SARD 15CU 72000 R 6220 L C CX007 129.9 7CU NALU 15CD SARD 17CU 36000 R 6280 L C C0017 129.9 17CU NALU 17CD NARD 19CU 36000 R 6320 L C C0002 129.9 2CU NBRU 2CD NBLD 21CU 36000 R 6360 L C C0004 129.9 4CU NBRU 4CD NBLD 23CU 41000 R 6402.5 L C C0006 129.9 6CU NBRU 6CD NBLD 2CU 72000 R 5970 R C C0008 129.9 8CU NBRU 8CD NBLD 4CU 72000 R 6050 R C CX002 129.9 2CU NBRU 10CD SBLD 6CU 72000 R 6130 R C CX004 129.9 4CU NBRU 12CD SBLD 8CU 72000 R 6220 R C CX006 129.9 6CU NBRU 14CD SBLD 10CU 72000 R 5970 R C CX008 129.9 8CU NBRU 16CD SBLD 12CU 72000 R 6050 R C C0018 129.9 18CU NBRU 18CD NBLD 14CU 72000 R 6130 R C C0009 129.9 9CU SALU 9CD SARD 16CU 72000 R 6220 R C C0011 129.9 11CU SALU 11CD SARD 18CU 36000 R 6280 R C C0013 129.9 13CU SALU 13CD SARD 20CU 36000 R 6320 R C C0015 129.9 15CU SALU 15CD SARD 22CU 36000 R 6360 R C CX009 129.9 9CU SALU 1CD NARD 24CU 41000 R 6402.5 R C CX011 129.9 11CU SALU 3CD NARD 1CD 72000 T 3745 R C CX013 129.9 13CU SALU 5CD NARD 3CD 72000 T 3825 R C CX015 129.9 15CU SALU 7CD NARD 5CD 72000 T 3905 R C CX017 129.9 17CU SALU 17CD SARD 7CD 72000 T 3995 R C C0010 129.9 10CU SBRU 10CD SBLD 9CD 72000 T 3745 R C C0012 129.9 12CU SBRU 12CD SBLD 11CD 72000 T 3825 R C C0014 129.9 14CU SBRU 14CD SBLD

13CD 72000 T 3905 R C C0016 129.9 16CU SBRU 16CD SBLD 15CD 72000 T 3995 R C CX010 129.9 10CU SBRU 2CD NBLD 17CD 36000 T 4055 R C CX012 129.9 12CU SBRU 4CD NBLD 19CD 36000 T 4095 R C CX014 129.9 14CU SBRU 6CD NBLD 21CD 36000 T 4135 R C CX016 129.9 16CU SBRU 8CD NBLD 23CD 41000 T 4177.5 R C CX018 129.9 18CU SBRU 18CD SBLD 2CD 72000 T 3745 L C CA017 130.5 17CU GALU 17CD GARD 4CD 72000 T 3825 L C CA019 130.5 19CU GALU 19CD GARD 6CD 72000 T 3905 L C CA021 130.5 21CU GALU 21CD GARD 8CD 72000 T 3995 L C CA023 130.5 23CU GALU 23CD GARD 10CD 72000 T 3745 L C CB018 130.5 18CU GBRU 18CD GBLD 12CD 72000 T 3825 L C CB020 130.5 20CU GBRU 20CD GBLD 14CD 72000 T 3905 L C CB022 130.5 22CU GBRU 22CD GBLD 16CD 72000 T 3995 L C CB024 130.5 24CU GBRU 24CD GBLD 18CD 36000 T 4055 L C K0001 134.8 1KU F1HU 1KD F1VD 20CD 36000 T 4095 L C K0003 134.8 3KU F1HU 3KD F1VD 22CD 36000 T 4135 L C K0005 134.8 5KU F1HU 5KD F1VD 24CD 41000 T 4177.5 L C K0007 134.8 7KU F1HU 7KD F1VD CMD1 1000 R 6173.7 L T K0009 134.8 9KU F1HU 9KD F1VD CMD2 1000 R 6176.3 L T K0011 134.8 11KU F1HU 11KD F1VD TLM1 500 T 3947.5 R T KX007 134.8 7KU F1HU 13KD F2VD TLM2 500 T 3952.5 R T KX009 134.8 9KU F1HU 15KD F2VD BNC1 25 T 3950 V T KX011 134.8 11KU F1HU 17KD F2VD BNK1 25 T 11198 R T FH007 134.8 7KU F2HU 7KD F1VD BNK2 25 T 11452 R T FH009 134.8 9KU F2HU 9KD F1VD BNK3 25 T 12502 R T FH011 134.8 11KU F2HU 11KD F1VD 1KU 72000 R 14045 H C FX007 134.8 7KU F2HU 13KD F2VD 3KU 72000 R 14125 H C FX009 134.8 9KU F2HU 15KD F2VD 5KU 72000 R 14205 H C FX011 134.8 11KU F2HU 17KD F2VD 7KU 72000 R 14295 H C FV002 134.8 2KU F2VU 2KD F2HD 9KU 72000 R 14375 H C FV004 134.8 4KU F2VU 4KD F2HD 11KU 72000 R 14455 H C FV006 134.8 6KU F2VU 6KD F2HD 2KU 72000 R 14045 V C FV008 134.8 8KU F2VU 8KD F2HD 4KU 72000 R 14125 V C FV010 134.8 10KU F2VU 10KD F2HD 6KU 72000 R 14205 V C FV012 134.8 12KU F2VU 12KD F2HD 8KU 72000 R 14295 V C FY002 134.8 2KU F2VU 14KD F2HD 10KU 72000 R 14375 V C FY004 134.8 4KU F2VU 16KD F2HD 12KU 72000 R 14455 V C FY006 134.8 6KU F2VU 18KD F2HD 1KD 72000 T 10995 V C FY008 134.8 8KU F2VU 20KD F2HD

3KD 72000 T 11075 V C FY010 134.8 10KU F2VU 22KD F2HD 5KD 72000 T 11155 V C FY012 134.8 12KU F2VU 24KD F2HD 7KD 72000 T 11495 V C U0002 134.8 2KU USVU 2KD F2HD 9KD 72000 T 11575 V C U0004 134.8 4KU USVU 4KD F2HD 11KD 72000 T 11655 V C U0006 134.8 6KU USVU 6KD F2HD 13KD 72000 T 12547 V C U0008 134.8 8KU USVU 8KD F2HD 15KD 72000 T 12627 V C U0010 134.8 10KU USVU 10KD F2HD 17KD 72000 T 12707 V C U0012 134.8 12KU USVU 12KD F2HD 2KD 72000 T 10995 H C UX002 134.8 2KU USVU 14KD F2HD 4KD 72000 T 11075 H C UX004 134.8 4KU USVU 16KD F2HD 6KD 72000 T 11155 H C UX006 134.8 6KU USVU 18KD F2HD 8KD 72000 T 11495 H C UX008 134.8 8KU USVU 20KD F2HD 10KD 72000 T 11575 H C UX010 134.8 10KU USVU 22KD F2HD 12KD 72000 T 11655 H C UX012 134.8 12KU USVU 24KD F2HD 14KD 72000 T 12297 H C 16KD 72000 T 12377 H C 18KD 72000 T 12457 H C 20KD 72000 T 12547 H C 22KD 72000 T 12627 H C 24KD 72000 T 12707 H 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) D1 72M0G7W 72000 4 49138 0.5 3.36 17.9 D2 36M0G7W 36000 4 24575 0.5 3.36 12.4 D3 10M3G7W 10300 4 6000 0.5 3.87 16.3 D4 100KG7W 100 4 64 0.5 2.99 15.6 D5 1M45G7W 1450 2 512 0.5 3.4 15.5 D6 400KG7W 400 2 128 0.5 3.4 14.9

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 22.2

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) C0001 UX012 A1 1 36000 INTELSAT 18 4000 58.4 18.1 24.1 35.3 41.3 -150.8 23.6 C0001 UX012 D2 1 36000 NOTE.txt 51 15.8 21.8 35.5 41.5 -159.4 19.2 C0001 UX012 D3 2 10300 NOTE.txt 51 9.6 15.6 28 34 -160.4 19.2 C0001 UX012 D4 276 100 NOTE.txt 51 -10.8 -4.8 7.6 13.6 -161.3 19.2 C0001 UX012 A1 2 36000 NOTE.txt 4000 56.4 18.4 24.4 30.2 36.2 -155.9 28.4 C0001 UX012 D1 1 72000 NOTE.txt 51 20.8 26.8 34.4 40.4 -163.5 19.2 C0001 UX012 D3 4 10300 NOTE.txt 51 8.8 14.8 24.1 30.1 -164.3 21 C0001 UX012 D4 527 100 NOTE.txt 51 -11.6 -5.6 3.7 9.7 -165.2 21 C0001 UX012 A1 2 36000 NOTE.txt 4000 58.4 18.9 24.9 31.3 37.3 -154.8 26.6 C0001 UX012 D1 1 72000 NOTE.txt 53.4 16.9 22.9 35.5 41.5 -162.4 19.2 C0001 UX012 D3 4 10300 NOTE.txt 51 14.3 20.3 25.3 31.3 -163.1 19.2 C0001 UX012 D4 518 100 NOTE.txt 51 -6.1 -0.1 4.8 10.8 -164.1 19.2 C0001 UX012 A1 1 36000 NOTE.txt 4000 55.4 17.9 23.9 34.4 40.4 -151.7 26.2 C0001 UX012 D2 1 36000 NOTE.txt 51 16.3 22.3 34.4 40.4 -160.5 19.2 C0001 UX012 D3 2 10300 NOTE.txt 51 10.3 16.3 27.1 33.1 -161.3 19.2 C0001 UX012 D4 264 100 NOTE.txt 51 -10.1 -4.1 6.7 12.7 -162.2 19.2 C0001 UX012 A1 1 36000 NOTE.txt 4000 58.4 18.7 22.7 30.9 34.9 -157.2 31 C0001 UX012 D2 1 36000 NOTE.txt 51 16.1 20.1 30.9 34.9 -166 23.6 C0001 UX012 D3 2 10300 NOTE.txt 51 14.1 18.1 23.6 27.6 -166.8 23.6 C0001 UX012 D4 262 100 NOTE.txt 51 -6.3 -2.3 3.2 7.2 -167.7 23.6 C0001 UX012 A1 2 36000 NOTE.txt 4000 56.9 17.2 23.2 42.4 48.4 -143.7 28.6 C0001 UX012 D1 1 72000 NOTE.txt 56.9 17.7 23.7 45.8 51.8 -152.1 22.3 C0001 UX012 D3 5 10300 NOTE.txt 56.9 9 15 34.5 40.5 -153.9 22.3 C0001 UX012 D4 526 100 NOTE.txt 56.9 -11.2 -5.2 14.3 20.3 -154.6 22.3 C0001 UX012 D5 33 1450 NOTE.txt 56.9 0.8 6.8 26.3 32.3 -154.7 22.3 C0001 UX012 D6 180 400 NOTE.txt 46.4 -3.9 2.1 11.1 17.1 -163.9 33.1

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, N.W. 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 1464 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1736 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3200 23.6 0.796 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 619 5.6 0.839 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 37.5 8.6 0.668 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): 4898 4898 4898 4898 Bus (Watts): (b): (g): (l): (q): 1345 753 1345 753 Total (Watts): (c): (h): (m): (r): 6243 5651 6243 5651 Solar Array (Watts): (d): (i): (n): (s): 6949 6386 6746 6114 Depth of Battery (e) (j) (o) (t) Discharge (%): 66.4 % % 67.2 % % 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: 2010-10-15 11:19:04
Document Modified: 2010-10-15 11:19:04
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