Attachment Schedule S Tech Data

This document pretains to SAT-RPL-20041015-00201 for Replacement Application on a Satellite Space Stations filing.

IBFS_SATRPL2004101500201_403533

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 AMERICAS-9 8/30/2008 Y b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 1/11/2004 13 Years 44 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 1/11/2007 44 1296 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: 1/1/2008 6/30/2008 1296 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 14 G 14.5 G R Fixed Satellite Service 11.7 G 12.2 G 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: 77 W Intelsat North America already holds an FCC Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be authorization to operate a satellite at this orbital N/S Station-Keeping provided (Optional): location. This application seeks authorization for a d. Toward West: Degrees E/W 0.05 Degrees Tolerance: replacement satellite in that same orbital location. g. Westernmost: 129 W e. Toward East: 0.05 Degrees 0.05 Degrees h. Easternmost: 77 W i. Reason for service are selection (Optional): The satellite Intelsat Americas-9 can replace any of the Intelsat 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 Area 1.gxt USA, CAN, DOM, HTI, MEX, VIR, PTR 2 S Service Area 2.gxt CLM, EQA, PRU, BOL, CHL, PRG, ARG, URG, B, VEN, GUF, SUR

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) CTF T 29.8 22.8 0.15 0.4 30 Y 01 3 14 43.8 CRF R 29.1 24.6 0.15 0.4 30 Y 0 1 483 0.8 -92 20 1 KTF T 31.6 24.4 0.15 0.4 30 N 0 1 3 18.3 49.9 KRF R 31.6 23.8 0.15 0.4 30 N 0 1 490 3.3 -96 20 1 KTR T 37 28.2 0.15 0.4 30 N 0 2 3 18.3 55.3 KRR R 36 26.9 0.15 0.4 30 N 02 768 7.7 -96 20 1

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) CTF T C 77 ctf_c.gxt -158.2 -158.2 -158.2 -158.2 -158.2 CTF T X 77 ctf_x.gxt CRF R C 77 crf_c.gxt CRF R X 77 crf_x.gxt KTF T C 77 ktf_c.gxt -150.9 -150.9 -150.9 -150.9 -150.9 KTF T X 77 KRF R C 77 KRF R X 77 KTR T C 77 ktr_c.gxt -146.7 -146.7 -146.7 -146.7 -146.7 KTR T X 77 ktr_x.gxt KRR R C 77 krr_c.gxt KRR R X 77 krr_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) CT1 36 T 3720 V C C1 148 CR1 CRF CT1 CTF CT2 36 T 3740 H C C2 148 CR2 CRF CT2 CTF CT3 36 T 3760 V C C3 148 CR3 CRF CT3 CTF CT4 36 T 3780 H C C4 148 CR4 CRF CT4 CTF CT5 36 T 3800 V C C5 148 CR5 CRF CT5 CTF CT6 36 T 3820 H C C6 148 CR6 CRF CT6 CTF CT7 36 T 3840 V C C7 148 CR7 CRF CT7 CTF CT8 36 T 3860 H C C8 148 CR8 CRF CT8 CTF CT9 36 T 3880 V C C9 148 CR9 CRF CT9 CTF CT10 36 T 3900 H C C10 148 CR10 CRF CT10 CTF CT11 36 T 3920 V C C11 148 CR11 CRF CT11 CTF CT12 36 T 3940 H C C12 148 CR12 CRF CT12 CTF CT13 36 T 3960 V C C13 148 CR13 CRF CT13 CTF CT14 36 T 3980 H C C14 148 CR14 CRF CT14 CTF CT15 36 T 4000 V C C15 148 CR15 CRF CT15 CTF CT16 36 T 4020 H C C16 148 CR16 CRF CT16 CTF CT17 36 T 4040 V C C17 148 CR17 CRF CT17 CTF CT18 36 T 4060 H C C18 148 CR18 CRF CT18 CTF CT19 36 T 4080 V C C19 148 CR19 CRF CT19 CTF CT20 36 T 4100 H C C20 148 CR20 CRF CT20 CTF CT21 36 T 4120 V C C21 148 CR21 CRF CT21 CTF CT22 36 T 4140 H C C22 148 CR22 CRF CT22 CTF CT23 36 T 4160 V C C23 148 CR23 CRF CT23 CTF CT24 36 T 4180 H C C24 148 CR24 CRF CT24 CTF CR1 36 R 5945 H C K1 159.1 KR1 KRF KT1 KTF CR2 36 R 5965 V C K2 159.1 KR2 KRF KT2 KTF CR3 36 R 5985 H C K3 159.1 KR3 KRF KT3 KTF CR4 36 R 6005 V C K4 159.1 KR4 KRF KT4 KTF CR5 36 R 6025 H C K5 159.1 KR5 KRF KT5 KTF CR6 36 R 6045 V C K6 159.1 KR6 KRF KT6 KTF

CR7 36 R 6065 H C K7 159.1 KR7 KRF KT7 KTF CR8 36 R 6085 V C K8 159.1 KR8 KRF KT8 KTF CR9 36 R 6105 H C K9 159.1 KR9 KRF KT9 KTF CR10 36 R 6125 V C K10 159.1 KR10 KRF KT10 KTF CR11 36 R 6145 H C K11 159.1 KR11 KRF KT11 KTF CR12 36 R 6165 V C K12 159.1 KR12 KRF KT12 KTF CR13 36 R 6185 H C K13 159.1 KR13 KRF KT13 KTF CR14 36 R 6205 V C K14 159.1 KR14 KRF KT14 KTF CR15 36 R 6225 H C K15 159.1 KR15 KRF KT15 KTF CR16 36 R 6245 V C K16 159.1 KR16 KRF KT16 KTF CR17 36 R 6265 H C K17 159.1 KR17 KRF KT17 KTF CR18 36 R 6285 V C K18 159.1 KR18 KRF KT18 KTF CR19 36 R 6305 H C K19 159.1 KR19 KRF KT19 KTF CR20 36 R 6325 V C K20 159.1 KR20 KRF KT20 KTF CR21 36 R 6345 H C K21 159.1 KR21 KRF KT21 KTF CR22 36 R 6365 V C K22 159.1 KR22 KRF KT22 KTF CR23 36 R 6385 H C K23 159.1 KR23 KRF KT23 KTF CR24 36 R 6405 V C K24 159.1 KR24 KRF KT24 KTF KT1 27 T 11715 V C K25 159.1 KR25 KRF KT25 KTF KT2 27 T 11721.5 H C K26 159.1 KR26 KRF KT26 KTF KT3 27 T 11745 V C K27 159.1 KR27 KRF KT27 KTF KT4 27 T 11751.5 H C K28 159.1 KR28 KRF KT28 KTF KT5 27 T 11775 V C K29 159.1 KR29 KRF KT29 KTF KT6 27 T 11781.5 H C K30 159.1 KR30 KRF KT30 KTF KT7 27 T 11805 V C K31 159.1 KR31 KRF KT31 KTF KT8 27 T 11811.5 H C K32 159.1 KR32 KRF KT32 KTF KT9 27 T 11836 V C S1 167.6 SR1 KRR ST1 KTR KT10 27 T 11842.5 H C S2 167.6 SR2 KRR ST2 KTR KT11 27 T 11867 V C S3 167.6 SR3 KRR ST3 KTR KT12 27 T 11873.5 H C S4 167.6 SR4 KRR ST4 KTR KT13 27 T 11898 V C S5 167.6 SR5 KRR ST5 KTR KT14 27 T 11904.5 H C S6 167.6 SR6 KRR ST6 KTR KT15 27 T 11929 V C KT16 27 T 11935.5 H C KT17 27 T 11960 V C KT18 27 T 11966.5 H C KT19 27 T 11991 V C KT20 27 T 11997.5 H C KT21 27 T 12022 V C

KT22 27 T 12028.5 H C KT23 27 T 12053 V C KT24 27 T 12059.5 H C KT25 27 T 12084 V C KT26 27 T 12090.5 H C KT27 27 T 12115 V C KT28 27 T 12121.5 H C KT29 27 T 12146 V C KT30 27 T 12152.5 H C KT31 27 T 12177 V C KT32 27 T 12183.5 H C KR1 27 R 14015 H C KR2 27 R 14021.5 V C KR3 27 R 14045 H C KR4 27 R 14051.5 V C KR5 27 R 14075 H C KR6 27 R 14081.5 V C KR7 27 R 14105 H C KR8 27 R 14111.5 V C KR9 27 R 14136 H C KR10 27 R 14142.5 V C KR11 27 R 14167 H C KR12 27 R 14173.5 V C KR13 27 R 14198 H C KR14 27 R 14204.5 V C KR15 27 R 14229 H C KR16 27 R 14235.5 V C KR17 27 R 14260 H C KR18 27 R 14266.5 V C KR19 27 R 14291 H C KR20 27 R 14297.5 V C KR21 27 R 14322 H C KR22 27 R 14328.5 V C KR23 27 R 14353 H C KR24 27 R 14359.5 V C KR25 27 R 14384 H C KR26 27 R 14390.5 V C KR27 27 R 14415 H C KR28 27 R 14421.5 V C

KR29 27 R 14446 H C KR30 27 R 14452.5 V C KR31 27 R 14477 H C KR32 27 R 14483.5 V C ST1 36 T 11725 V C ST2 36 T 11765 V C ST3 36 T 11805 V C ST4 36 T 11845 V C ST5 36 T 11885 V C ST6 36 T 11925 V C SR1 36 R 14025 H C SR2 36 R 14065 H C SR3 36 R 14105 H C SR4 36 R 14145 H C SR5 36 R 14185 H C SR6 36 R 14225 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) 1 67K5G1W 67.5 8 64 0.6667 10.5 22.7 2 203KG1W 202.5 8 256 0.6667 10.5 22.7 3 833KG1W 832.5 8 1024 0.6667 10.5 22.7 4 1M28G7W 1282.5 8 1544 0.6667 10.5 22.7 5 4M93G7W 4927.5 8 6312 0.6667 10.5 22.7 6 6M55G7W 6547.5 8 8448 0.6667 10.5 22.7 7 24M6G7W 24625 8 32064 0.6667 10.5 22.7 8 26M4G7W 34250 8 34368 0.6667 10.5 22.7 9 113KG1W 112.5 4 64 0.5 4.9 17.1 10 788KG1W 787.5 4 512 0.5 4.9 17.1 11 245KG7W 2452.5 4 1544 0.5 4.9 17.1 12 3M13G7W 3127.5 4 2048 0.5 4.9 17.1 13 9M70G7W 9697.5 4 6312 0.5 4.9 17.1 14 12M9G7W 12892.5 4 8448 0.5 4.9 17.1

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) 1 20M0F3F 20000 TV/FM 1 NTSC 2.5 2.4 15.5 27.7 2 30M0F3F 30000 TV/FM 1 NTSC 2.5 2.4 17.2 29.4

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) C1 C24 1 2 36000 Link Budget 8000 54.1 27 27 41.8 43.8 -152.49 29.3 C1 C24 2 2 18000 Link Budget 4000 54.1 27 27 36.3 38.3 -154.99 29.3 C1 C24 1 465 Link Budget 54.1 -10.9 -2.6 11.1 13.1 -160.75 23.3 C1 C24 2 116 Link Budget 54.1 -4.9 3.4 17.1 19.1 -160.75 23.3 C1 C24 3 29 Link Budget 54.1 1.1 9.4 23.1 25.1 -160.75 23.3 C1 C24 4 19 Link Budget 54.1 2.9 11.2 24.9 26.9 -160.75 23.3 C1 C24 5 5 Link Budget 54.1 9 17.3 31 33 -160.75 23.3 C1 C24 6 4 Link Budget 54.1 10.3 18.6 32.3 34.3 -160.75 23.3 C1 C24 7 1 Link Budget 54.1 16.1 24.4 38.1 40.1 -160.75 23.3 C1 C24 8 1 Link Budget 54.1 16.4 24.7 38.4 40.4 -160.75 23.3 C1 C24 9 233 Link Budget 54.1 -7.9 0.4 14.1 16.1 -158.03 19.8 C1 C24 10 29 Link Budget 54.1 1.1 9.4 23.1 25.1 -158.03 19.8 C1 C24 11 10 Link Budget 54.1 5.9 14.2 27.9 29.9 -158.03 19.8 C1 C24 12 7 Link Budget 54.1 7.2 15.5 29.2 31.2 -158.03 19.8 C1 C24 13 2 Link Budget 54.1 12 20.3 34 36 -158.03 19.8 C1 C24 14 2 Link Budget 54.1 13.3 21.6 35.3 37.3 -158.03 19.8 K1 K32 1 300 Link Budget 60.3 -12.7 -4.5 19.1 21.1 -152.75 27.3 K1 K32 2 75 Link Budget 60.3 -6.7 1.5 25.1 27.1 -152.75 27.3 K1 K32 3 19 Link Budget 60.3 -0.7 7.5 31.1 33.1 -152.75 27.3 K1 K32 4 12 Link Budget 60.3 1.1 9.3 32.9 34.9 -152.75 27.3 K1 K32 5 3 Link Budget 60.3 7.2 15.4 39 41 -152.75 27.3 K1 K32 6 2 Link Budget 60.3 8.5 16.7 40.3 42.3 -152.75 27.3 K1 K32 7 1 Link Budget 60.3 14.3 22.5 46.1 48.1 -152.75 27.3 K1 K32 8 1 Link Budget 60.3 14.6 22.8 46.4 48.4 -152.75 27.3 K1 K32 9 189 Link Budget 61.3 -9.8 -1.6 21.1 23.1 -151.03 21.3 K1 K32 10 24 Link Budget 61.3 -0.8 7.4 30.1 32.1 -151.03 21.3 K1 K32 11 8 Link Budget 61.3 4 12.2 34.9 36.9 -151.03 21.3 K1 K32 12 6 Link Budget 61.3 5.3 13.5 36.2 38.2 -151.03 21.3 K1 K32 13 2 Link Budget 61.3 10.1 18.3 41 43 -151.03 21.3

K1 K32 14 1 Link Budget 61.3 11.4 19.6 42.3 44.3 -151.03 21.3 S1 S6 1 720 Link Budget 60.3 -13.1 -2.8 19.7 22.7 -151.15 27.3 S1 S6 2 180 Link Budget 60.3 -7.1 3.2 25.7 28.7 -151.15 27.3 S1 S6 3 45 Link Budget 60.3 -1.1 9.2 31.7 34.7 -151.15 27.3 S1 S6 4 30 Link Budget 60.3 0.7 11 33.5 36.5 -151.15 27.3 S1 S6 5 7 Link Budget 60.3 6.8 17.1 39.6 42.6 -151.15 27.3 S1 S6 6 5 Link Budget 60.3 8.1 18.4 40.9 43.9 -151.15 27.3 S1 S6 7 1 Link Budget 60.3 13.9 24.2 46.7 49.7 -151.15 27.3 S1 S6 8 1 Link Budget 60.3 14.2 24.5 47 50 -151.15 27.3 S1 S6 9 443 Link Budget 61.3 -10.1 0.2 21.8 24.8 -149.33 21.3 S1 S6 10 55 Link Budget 61.3 -1.1 9.2 30.8 33.8 -149.33 21.3 S1 S6 11 18 Link Budget 61.3 3.7 14 35.6 38.6 -149.33 21.3 S1 S6 12 14 Link Budget 61.3 5 15.3 36.9 39.9 -149.33 21.3 S1 S6 13 4 Link Budget 61.3 9.8 20.1 41.7 44.7 -149.33 21.3 S1 S6 14 3 LInk Budget 61.3 11.1 21.4 43 46 -149.33 21.3

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 Blvd S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Hagerstown 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 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 2464 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3164 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5610 8.72 0.83 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 956 4.83 0.87 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 56 5.97 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): 8355 8355 8355 8355 Bus (Watts): (b): (g): (l): (q): 2741 1536 2741 1536 Total (Watts): (c): (h): (m): (r): 11096 9891 11096 9891 Solar Array (Watts): (d): (i): (n): (s): 12655 11403 12075 10531 Depth of Battery (e) (j) (o) (t) Discharge (%): 77 % 77 % 76.1 % 76.1 % 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: 2004-11-02 06:11:17
Document Modified: 2004-11-02 06:11:17
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