Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20060816-00088 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2006081600088_520812

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-5 3/31/2008 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 4/1/1995 12 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 4/1/1997 52 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: 5/24/1997 5/24/1997 1728 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: 76.7 W Intelsat North America had an FCC authorization to Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be operate a satellite at the orbital location 77W and had N/S Station-Keeping provided (Optional): plans to deploy a satellite there. A co-location d. Toward West: Degrees E/W 0.05 Degrees Tolerance: agreement recently concluded with respect to an g. Westernmost: 129 W e. Toward East: 0.05 Degrees existing satellite (Echostar) as well as the planned 0.05 Degrees h. Easternmost: 77 W operation of Galaxy 4R at 76.85W requires Intelsat North America to locate its satellite at 76.7W instead i. Reason for service are selection (Optional): of 77W The Intelsat Americas-5 (IA-5) satellite can replace any of Intelsat's US licensed spacecraft located within this arc in case of catastrophic 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 area1.gxt USA, CAN, DOM, HTI, MEX, VIR, PTR, CUB 2 S Service area2-76_7W.g 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) CTF T 29.3 22.6 0.1 0.4 30 Y 01 2 12.6 40.3 CRF R 30.7 21.7 0.1 0.4 30 Y 0 1 646 2.6 -92 21 1 KTF T 32.3 25.2 0.1 0.4 30 N 0 1 1.5 70.8 50.8 KRF R 30.9 26.3 0.2 0.4 30 N 0 1 661 2.7 -96 21 1 O-R R 2 0 0.1 0.4 20 N 0 2 500 -25 O-T T 2 0 0.1 0.4 20 N 02 7.6 3.5 7.4

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 IA5_nactco.gxt -159.4 -159.4 -159.4 -159.4 -159.4 CTF T X -77 IA5_nactxp.gxt KTF T C -77 IA5_naktco.gxt -149.5 -149.5 -149.5 -149.5 -149.5 KTF T X -77 IA5_naktxp.gxt CRF R C -77 IA5_nacrco.gxt CRF R X -77 IA5_nacrxp.gxt KRF R C -77 IA5_nakrco.gxt KRF R X -77 IA5_nakrxp.gxt O-R R C -77 O.gxt O-T T C -77 O-E.gxt -172.1 -172.1 -172.1 -172.1 -172.1

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 36000 T 3720 V C C1 110.7 CR1 CRF CT1 CTF CT2 36000 T 3740 H C C2 110.7 CR2 CRF CT2 CTF CT3 36000 T 3760 V C C3 110.7 CR3 CRF CT3 CTF CT4 36000 T 3780 H C C4 110.7 CR4 CRF CT4 CTF CT5 36000 T 3800 V C C5 110.7 CR5 CRF CT5 CTF CT6 36000 T 3820 H C C6 110.7 CR6 CRF CT6 CTF CT7 36000 T 3840 V C C7 110.7 CR7 CRF CT7 CTF CT8 36000 T 3860 H C C8 110.7 CR8 CRF CT8 CTF CT9 36000 T 3880 V C C9 110.7 CR9 CRF CT9 CTF CT10 36000 T 3900 H C C10 110.7 CR10 CRF CT10 CTF CT11 36000 T 3920 V C C11 110.7 CR11 CRF CT11 CTF CT12 36000 T 3940 H C C12 110.7 CR12 CRF CT12 CTF CT13 36000 T 3960 V C C13 110.7 CR13 CRF CT13 CTF CT14 36000 T 3980 H C C14 110.7 CR14 CRF CT14 CTF CT15 36000 T 4000 V C C15 110.7 CR15 CRF CT15 CTF CT16 36000 T 4020 H C C16 110.7 CR16 CRF CT16 CTF CT17 36000 T 4040 V C C17 110.7 CR17 CRF CT17 CTF CT18 36000 T 4060 H C C18 110.7 CR18 CRF CT18 CTF CT19 36000 T 4080 V C C19 110.7 CR19 CRF CT19 CTF CT20 36000 T 4100 H C C20 110.7 CR20 CRF CT20 CTF CT21 36000 T 4120 V C C21 110.7 CR21 CRF CT21 CTF CT22 36000 T 4140 H C C22 110.7 CR22 CRF CT22 CTF CT23 36000 T 4160 V C C23 110.7 CR23 CRF CT23 CTF CT24 36000 T 4180 H C C24 110.7 CR24 CRF CT24 CTF KT1 54000 T 11728.5 V C K1 129.3 KR1 KRF KT1 KTF KT2 54000 T 11735 H C K2 129.3 KR2 KRF KT2 KTF KT3 54000 T 11789.5 V C K3 129.3 KR3 KRF KT3 KTF KT4 54000 T 11796 H C K4 129.3 KR4 KRF KT4 KTF KT5 27000 T 11836 V C K5 129.3 KR5 KRF KT5 KTF KT6 27000 T 11842.5 H C K6 129.3 KR6 KRF KT6 KTF

KT7 27000 T 11867 V C K7 129.3 KR7 KRF KT7 KTF KT8 27000 T 11873.5 H C K8 129.3 KR8 KRF KT8 KTF KT9 27000 T 11898 V C K9 129.3 KR9 KRF KT9 KTF KT10 27000 T 11904.5 H C K10 129.3 KR10 KRF KT10 KTF KT11 27000 T 11929 V C K11 129.3 KR11 KRF KT11 KTF KT12 27000 T 11935.5 H C K12 129.3 KR12 KRF KT12 KTF KT13 27000 T 11960 V C K13 129.3 KR13 KRF KT13 KTF KT14 27000 T 11966.5 H C K14 129.3 KR14 KRF KT14 KTF KT15 27000 T 11991 V C K15 129.3 KR15 KRF KT15 KTF KT16 27000 T 11997.5 H C K16 129.3 KR16 KRF KT16 KTF KT17 27000 T 12022 V C K17 129.3 KR17 KRF KT17 KTF KT18 27000 T 12028.5 H C K18 129.3 KR18 KRF KT18 KTF KT19 27000 T 12053 V C K19 129.3 KR19 KRF KT19 KTF KT20 27000 T 12059.5 H C K20 129.3 KR20 KRF KT20 KTF KT21 27000 T 12084 V C K21 129.3 KR21 KRF KT21 KTF KT22 27000 T 12090.5 H C K22 129.3 KR22 KRF KT22 KTF KT23 27000 T 12115 V C K23 129.3 KR23 KRF KT23 KTF KT24 27000 T 12121.5 H C K24 129.3 KR24 KRF KT23 KTF KT25 27000 T 12146 V C K25 129.3 KR25 KRF KT24 KTF KT26 27000 T 12152.5 H C K26 129.3 KR26 KRF KT26 KTF KT27 27000 T 12177 V C K27 129.3 KR27 KRF KT27 KTF KT28 27000 T 12183.5 H C K28 129.3 KR28 KRF KT28 KTF TLC1 1000 R 5925.5 V T TLC2 1000 R 6424.5 H T TLM1 100 T 4198 V T TLM2 100 T 4198.5 V T TLM3 100 T 4199 V T TLM4 100 T 4199.5 V T TLM5 100 T 11702 H T TLM6 100 T 12198 V T CR1 36000 R 5945 H C CR2 36000 R 5965 V C CR3 36000 R 5985 H C CR4 36000 R 6005 V C CR5 36000 R 6025 H C CR6 36000 R 6045 V C CR7 36000 R 6065 H C CR8 36000 R 6085 V C CR9 36000 R 6105 H C

CR10 36000 R 6125 V C CR11 36000 R 6145 H C CR12 36000 R 6165 V C CR13 36000 R 6185 H C CR14 36000 R 6205 V C CR15 36000 R 6225 H C CR16 36000 R 6245 V C CR17 36000 R 6265 H C CR18 36000 R 6285 V C CR19 36000 R 6305 H C CR20 36000 R 6325 V C CR21 36000 R 6345 H C CR22 36000 R 6365 V C CR23 36000 R 6385 H C CR24 36000 R 6405 V C KR1 54000 R 14028.5 H C KR2 54000 R 14035 V C KR3 54000 R 14089.5 H C KR4 54000 R 14096 V C KR5 27000 R 14136 H C KR6 27000 R 14142.5 V C KR7 27000 R 14167 H C KR8 27000 R 14173.5 V C KR9 27000 R 14198 H C KR10 27000 R 14204.5 V C KR11 27000 R 14229 H C KR12 27000 R 14235.5 V C KR13 27000 R 14260 H C KR14 27000 R 14266.5 V C KR15 27000 R 14291 H C KR16 27000 R 14297.5 V C KR17 27000 R 14322 H C KR18 27000 R 14328.5 V C KR19 27000 R 14353 H C KR20 27000 R 14359.5 V C KR21 27000 R 14384 H C KR22 27000 R 14390.5 V C KR23 27000 R 14415 H C KR24 27000 R 14421.5 V C

KR25 27000 R 14446 H C KR26 27000 R 14452.5 V C KR27 27000 R 14477 H C KR28 27000 R 14483.5 V 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 47K1G1W 47.1 8 64 0.6667 14.5 22.7 2 188KG1W 188.2 8 256 0.6667 14.5 26.7 3 753KG1W 752.9 8 1024 0.6667 14.5 26.7 4 1M13G7W 1135.3 8 1544 0.6667 14.5 26.7 5 4M64G7W 4641.2 8 6312 0.6667 14.5 26.7 6 6M21G7W 6211.8 8 8448 0.6667 14.5 26.7 7 23M6G7W 23576.5 8 32064 0.6667 14.5 26.7 8 25M3G7W 25270.6 8 34368 0.6667 14.5 26.7 9 94K1G1W 94.1 4 64 0.5 7.8 20 10 753KG1W 752.9 4 512 0.5 7.8 20 11 2M27G7W 2270.6 4 1544 0.5 7.8 20 12 3M65G7W 3652.9 4 2484 0.5 7.8 20 13 9M28G7W 9282.4 4 6312 0.5 7.8 20 14 12M4G7W 12423.5 4 8448 0.5 7.8 20

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 20M0F8W 20000 TV/FM 1 NTSC 2.5 2.4 17.5 31.5 2 30M0F8W 30000 TV/FM 1 NTSC 2.5 2.4 19.2 33.2 3 1M00F9D 1000 7 21 4 200KG8X 200 7 21 5 200KF9D 200 7 21 6 25K0N0N 25 7 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) C1 C24 1 1 Link_budget_T 2000 57.8 21.6 26.5 38.1 40.3 -149.2 31 C1 C24 2 2 18000 Link_budget_T 2000 57.8 22.6 26.5 32.6 34.8 -154.7 31 C1 C24 1 307 47.1 Link_budget_C 46.8 -2.3 6.7 5.7 12.4 -159.5 26.6 C1 C24 2 77 188.2 Link_budget_C 46.8 3.7 12.7 11.7 18.4 -159.5 26.6 C1 C24 3 19 752.9 Link_budget_C 46.8 9.7 18.7 17.7 24.4 -159.5 26.6 C1 C24 4 13 1135.3 Link_budget_C 46.8 11.5 20.5 19.5 26.2 -159.5 26.6 C1 C24 5 3 4641.2 Link_budget_C 46.8 17.6 26.6 25.6 32.3 -159.5 26.6 C1 C24 6 2 6211.8 Link_budget_C 46.8 18.9 27.9 26.9 33.6 -159.5 26.6 C1 C24 7 1 Link_budget_C 46.8 24.7 33.7 32.7 39.4 -159.5 26.6 C1 C24 8 1 Link_budget_C 46.8 25 34 33 39.7 -159.5 26.6 C1 C24 9 153 94.1 Link_budget_C 46.8 -6 3.2 8.8 15.5 -159.4 24.1 C1 C24 10 19 752.9 Link_budget_C 46.8 3 12.2 17.8 24.5 -159.4 24.1 C1 C24 11 6 2270.6 Link_budget_C 46.8 7.8 17 22.6 29.3 -159.4 24.1 C1 C24 12 4 3652.9 Link_budget_C 46.8 9.9 19.1 24.7 31.4 -159.4 24.1 C1 C24 13 2 9282.4 Link_budget_C 46.8 13.9 23.1 28.7 35.4 -159.4 24.1 C1 C24 14 1 12423.5 Link_budget_C 46.8 15.2 24.4 30 36.7 -159.4 24.1 K1 K28 1 764 47.1 Link_budget_K 52.7 -12.1 -4.6 8.4 15.5 -156.4 30.9 K1 K28 2 191 188.2 Link_budget_K 52.7 -6.1 1.4 14.4 21.5 -156.4 30.9 K1 K28 3 48 752.9 Link_budget_K 52.7 -0.1 7.4 20.4 27.5 -156.4 30.9 K1 K28 4 32 1135.3 Link_budget_K 52.7 1.7 9.2 22.2 29.3 -156.4 30.9 K1 K28 5 8 4641.2 Link_budget_K 52.7 7.8 15.3 28.3 35.4 -156.4 30.9 K1 K28 6 6 6211.8 Link_budget_K 52.7 9.1 16.6 29.6 36.7 -156.4 30.9 K1 K28 7 2 Link_budget_K 52.7 14.9 22.4 35.4 42.5 -156.4 30.9 K1 K28 8 1 Link_budget_K 52.7 15.2 22.7 35.7 42.8 -156.4 30.9 K1 K28 9 382 94.1 Link_budget_K 52.7 -15.4 -1.6 11.4 18.5 -156.4 24.4 K1 K28 10 48 752.9 Link_budget_K 52.7 -6.4 7.4 20.4 27.5 -156.4 24.4 K1 K28 11 16 2270.6 Link_budget_K 52.7 -1.6 12.2 25.2 32.3 -156.4 24.4 K1 K28 12 10 3652.9 Link_budget_K 52.7 0.5 14.3 27.3 34.4 -156.4 24.4 K1 K28 13 4 Link_budget_K 52.7 4.5 18.3 31.3 38.4 -156.4 24.4

K1 K28 14 3 Link_budget_K 52.7 5.8 19.6 32.6 39.7 -156.4 24.4

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: 22401 Juniper lats Road S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Nuevo Riverside CA 92567 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 909-928-3446 E040125 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 KA275

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 1469 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2191 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3660 31.1 0.8773 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 942 8.64 0.8492 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 59.61 5.79 0.745 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): 6303 6303 6303 6303 Bus (Watts): (b): (g): (l): (q): 1588 798 1588 798 Total (Watts): (c): (h): (m): (r): 7891 7101 7891 7101 Solar Array (Watts): (d): (i): (n): (s): 9906 8858 8212 7501 Depth of Battery (e) (j) (o) (t) Discharge (%): % % % % 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: 2006-08-17 11:55:00
Document Modified: 2006-08-17 11:55:00
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