Attachment Schedule S Tech Data

This document pretains to SAT-AMD-20080617-00124 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2008061700124_648833

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: GALAXY BSS-2 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 45 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: 1656 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 17/24 GHz BSS 17.3 G 17.8 G T 17/24 GHz BSS 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: 95.15 W The grid orbital location of 95W is already used by Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Intelsat (possibility of multi-band payloads). The 0.15 N/S Station-Keeping provided (Optional): degree offset is required because of satellites currently d. Toward West: Degrees E/W 0.05 Degrees Tolerance: in orbit. 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 United States 2 S South America 3 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) NRFL R 35.5 25.5 0.15 0.15 25 N 1 795 6.5 -100 25 1 NRF R 35.5 25.5 0.15 0.15 25 N 1 795 6.5 -100 25 1 SRF R 35.5 25.5 0.15 0.15 25 N 2 795 6.5 -100 25 1 GR R 46.1 40.1 0.075 0.075 25 N 1 915 16.5 -110 25 1 NTFL T 34.5 28.5 0.15 0.15 25 N 1 1.6 89.1 54 NTF T 34.5 28.5 0.15 0.15 25 N 1 1.6 89.1 54 STF T 32 26 0.15 0.15 25 N 2 1 631 60 UT T 46.1 40.1 0.075 0.075 25 N 1 1.9 49 63 CMR R 35.5 25.5 0.15 0.15 N 1 5157 -1.6 -118.5 CML R 35.5 25.5 0.15 0.15 N 1 5157 -1.6 -118.5 CMH R 20.2 17.2 0.15 0.15 N 03 745 -8.5 -118.5 CMV R 20.2 17.2 0.15 0.15 N 90 3 745 -8.5 -118.5 TMR T 34.5 24.5 0.15 0.15 N 1 1.5 0.28 29 TML T 34.5 24.5 0.15 0.15 N 1 1.5 0.28 29 TMV T 20 17 0.15 0.15 N 90 3 2 0.63 18 PBR T 34.5 24.5 0.15 0.15 N 1 2.5 0.22 28 PBL T 34.5 24.5 0.15 0.15 N 1 2.5 0.22 28

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) NRFL R C -95.15 NRFL.gxt NRF R C -95.15 NRFR.gxt SRF R C -95.15 SRF.gxt GR R C -95.15 GR.gxt NTFL T C -95.15 NTFL.gxt -122.3 -122.2 -122.1 -121.9 -121.8 NTF T C -95.15 NTFR.gxt -122.3 -122.2 -122.1 -121.9 -121.8 STF T C -95.15 STF.gxt -116.3 -116.2 -116.1 -115.9 -115.8 UT T C -95.15 UT.gxt -116.3 -116.2 -116.1 -116 -115.8 CMR R C -95.15 CMR.gxt CML R C -95.15 CML.gxt CMH R C -95.15 CMH.gxt CMV R C -95.15 CMV.gxt TMR T C -95.15 TMR.gxt -128.3 -128.1 -128 -127.9 -127.8 TML T C -95.15 TML.gxt -128.3 -128.1 -128 -127.9 -127.8 TMV T C -95.15 TMV.gxt -163.2 -163.1 -163 -162.9 -162.8 PBR T C -95.15 PBR.gxt -122.3 -122.1 -122 -121.9 -121.8 PBL T C -95.15 PBL.gxt -122.3 -122.1 -122 -121.9 -121.8

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) GA001 48000 R 24802.66 L C NT001 133.4 NR001 NRFR NT001 NTFL GA002 48000 R 24860.98 L C NT003 133.4 NR003 NRFR NT003 NTFL GA003 48000 R 24919.3 L C NT005 133.4 NR005 NRFR NT005 NTFL GA004 48000 R 24977.62 L C NT007 133.4 NR007 NRFR NT007 NTFL GB001 48000 R 24802.66 L C NT009 133.4 NR009 NRFR NT009 NTFL GB002 48000 R 24860.98 L C NT011 133.4 NR011 NRFR NT011 NTFL GB003 48000 R 24919.3 L C NT013 133.4 NR013 NRFR NT013 NTFL GB004 48000 R 24977.62 L C NT015 133.4 NR015 NRFR NT015 NTFL GC001 48000 R 24802.66 L C NT017 133.4 NR017 NRFR NT017 NTFL GC002 48000 R 24860.98 L C NT019 133.4 NR019 NRFR NT019 NTFL GC003 48000 R 24919.3 L C NT021 133.4 NR021 NRFR NT021 NTFL GC004 48000 R 24977.62 L C NT023 133.4 NR023 NRFR NT023 NTFL GD001 48000 R 24802.66 L C NT025 133.4 NR025 NRFR NT025 NTFL GD002 48000 R 24860.98 L C NT002 133.4 NR002 NRFL NT002 NTFR GD003 48000 R 24919.3 L C NT004 133.4 NR004 NRFL NT004 NTFR GD004 48000 R 24977.62 L C NT006 133.4 NR006 NRFL NT006 NTFR GE001 48000 R 24802.66 L C NT008 133.4 NR008 NRFL NT008 NTFR GE002 48000 R 24860.98 L C NT010 133.4 NR010 NRFL NT010 NTFR GE003 48000 R 24919.3 L C A0001 130.2 GA001 GR UA001 UT GE004 48000 R 24977.62 L C A0002 130.2 GA002 GR UA002 UT GF001 48000 R 24802.66 L C A0003 130.2 GA003 GR UA003 UT GF002 48000 R 24860.98 L C A0004 130.2 GA004 GR UA004 UT GF003 48000 R 24919.3 L C B0001 130.2 GB001 GR UB001 UT GF004 48000 R 24977.62 L C B0002 130.2 GB002 GR UB002 UT UA001 48000 T 17352.66 R C B0003 130.2 GB003 GR UB003 UT UA002 48000 T 17410.98 R C B0004 130.2 GB004 GR UB004 UT UA003 48000 T 17469.3 R C C0001 130.2 GC001 GR UC001 UT UA004 48000 T 17527.62 R C C0002 130.2 GC002 GR UC002 UT UB001 48000 T 17352.66 R C C0003 130.2 GC003 GR UC003 UT UB002 48000 T 17410.98 R C C0004 130.2 GC004 GR UC004 UT

UB003 48000 T 17469.3 R C D0001 130.2 GD001 GR UD001 UT UB004 48000 T 17527.62 R C D0002 130.2 GD002 GR UD002 UT UC001 48000 T 17352.66 R C D0003 130.2 GD003 GR UD003 UT UC002 48000 T 17410.98 R C D0004 130.2 GD004 GR UD004 UT UC003 48000 T 17469.3 R C E0001 130.2 GE001 GR UE001 UT UC004 48000 T 17527.62 R C E0002 130.2 GE002 GR UE002 UT UD001 48000 T 17352.66 R C E0003 130.2 GE003 GR UE003 UT UD002 48000 T 17410.98 R C E0004 130.2 GE004 GR UE004 UT UD003 48000 T 17469.3 R C F0001 130.2 GF001 GR UF001 UT UD004 48000 T 17527.62 R C F0002 130.2 GF002 GR UF002 UT UE001 48000 T 17352.66 R C F0003 130.2 GF003 GR UF003 UT UE002 48000 T 17410.98 R C NT012 133.4 NR012 NRFL NT012 NTFR UE003 48000 T 17469.3 R C NT014 133.4 NR014 NRFL NT014 NTFR UE004 48000 T 17527.62 R C NT016 133.4 NR016 NRFL NT016 NTFR UF001 48000 T 17352.66 R C NT018 133.4 NR018 NRFL NT018 NTFR UF002 48000 T 17410.98 R C NT020 133.4 NR020 NRFL NT020 NTFR UF003 48000 T 17469.3 R C NT022 133.4 NR022 NRFL NT022 NTFR UF004 48000 T 17527.62 R C NT024 133.4 NR024 NRFL NT024 NTFR NR001 24000 R 24773.5 R C NT026 133.4 NR026 NRFL NT026 NTFR NR003 24000 R 24802.66 R C ST018 141.9 SR018 SRF ST018 STF NR005 24000 R 24831.82 R C ST020 141.9 SR020 SRF ST020 STF NR007 24000 R 24860.98 R C ST022 141.9 SR022 SRF ST022 STF NR009 24000 R 24890.14 R C ST024 141.9 SR024 SRF ST024 STF NR011 24000 R 24919.3 R C ST026 141.9 SR026 SRF ST026 STF NR013 24000 R 24948.46 R C ST028 141.9 SR028 SRF ST028 STF NR015 24000 R 24977.62 R C ST030 141.9 SR030 SRF ST030 STF NR017 24000 R 25006.78 R C ST032 141.9 SR032 SRF ST032 STF NR019 24000 R 25035.94 R C SF018 141.9 NR018 NRFL ST018 STF NR021 24000 R 25065.1 R C SF020 141.9 NR020 NRFL ST020 STF NR023 24000 R 25094.26 R C SF022 141.9 NR022 NRFL ST022 STF NR025 24000 R 25123.42 R C SF024 141.9 NR024 NRFL ST024 STF NR002 24000 R 24788.08 L C SF026 141.9 NR026 NRFL ST026 STF NR004 24000 R 24817.24 L C SF028 141.9 NR028 NRFL ST028 STF NR006 24000 R 24846.4 L C SF030 141.9 NR030 NRFL ST030 STF NR008 24000 R 24875.56 L C SF032 141.9 NR032 NRFL ST032 STF NR010 24000 R 24904.72 L C F0004 130.2 GF004 GR UF004 UT NR012 24000 R 24933.88 L C TLM1 TM1 TMR NR014 24000 R 24963.04 L C TLM2 TM2 TML NR016 24000 R 24992.2 L C TLM3 TM3 TMV

NR018 24000 R 25021.36 L C TLM4 TM4 TMV NR020 24000 R 25050.52 L C ULP1 UPC1 PBR NR022 24000 R 25079.68 L C ULP2 UPC2 PBL NR024 24000 R 25108.84 L C CM1 CMD1 CMR NR026 24000 R 25138 L C CM2 CMD2 CML NR028 24000 R 25167.16 L C CM3 CMD3 CMV NR030 24000 R 25196.32 L C CM4 CMD4 CMH NR032 24000 R 25225.48 L C SR018 24000 R 25021.36 L C SR020 24000 R 25050.52 L C SR022 24000 R 25079.68 L C SR024 24000 R 25108.84 L C SR026 24000 R 25138 L C SR028 24000 R 25167.16 L C SR030 24000 R 25196.32 L C SR032 24000 R 25225.48 L C NT001 24000 T 17323.5 L C NT003 24000 T 17352.66 L C NT005 24000 T 17381.82 L C NT007 24000 T 17410.98 L C NT009 24000 T 17440.14 L C NT011 24000 T 17469.3 L C NT013 24000 T 17498.46 L C NT015 24000 T 17527.62 L C NT017 24000 T 17556.78 L C NT019 24000 T 17585.94 L C NT021 24000 T 17615.1 L C NT023 24000 T 17644.26 L C NT025 24000 T 17673.42 L C NT002 24000 T 17338.08 R C NT004 24000 T 17367.24 R C NT006 24000 T 17396.4 R C NT008 24000 T 17425.56 R C NT010 24000 T 17454.72 R C NT012 24000 T 17483.88 R C NT014 24000 T 17513.04 R C NT016 24000 T 17542.2 R C NT018 24000 T 17571.36 R C NT020 24000 T 17600.52 R C

NT022 24000 T 17629.68 R C NT024 24000 T 17658.84 R C NT026 24000 T 17688 R C ST018 24000 T 17571.36 R C ST020 24000 T 17600.52 R C ST022 24000 T 17629.68 R C ST024 24000 T 17658.84 R C ST026 24000 T 17688 R C ST028 24000 T 17717.16 R C ST030 24000 T 17746.32 R C ST032 24000 T 17775.48 R C CMD1 1000 R 24751.5 R T CMD2 1000 R 25248.5 L T CMD3 1000 R 5925.5 V T CMD4 1000 R 6424.5 H T TM1 350 T 17303.0 R T TM2 350 T 17303.5 L T TM3 350 T 4197 V T TM4 350 T 4198.5 V T UPC1 50 T 17301 R T UPC2 50 T 17301.5 L 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 48M0G7W 40000 8 100000 0.83 8.9 26.1 2 24M0G7W 19988 4 26650 0.67 4.1 19.3 3 360KG7W 360 2 128 0.5 2.7 38.3

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 250KG7D 250 SCPC/FM 1 0.74 13.9 26.1 2 50K0G7X 50 SCPC/FM 1 0.74 4 16.2 3 860KF3D 860 SCPC/FM 1 13.3 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) NT001 NT026 2 1 GBSS2-LINK B 65.2 14 14 52 54 -121.8 16.2 NT001 NT026 3 66 360 GBSS2-LINK B 42.8 -2.8 -2.8 27.7 29.7 -127.4 39 ST018 ST032 2 1 GBSS2-LINK B 65.2 14 14 58 60 -115.8 13 ST018 ST032 3 66 360 GBSS2-LINK B 42.8 -2.8 -2.8 33.7 35.7 -121.4 39 SF018 SF032 2 1 GBSS2-LINK B 65.2 14 14 58 60 -115.8 13 A0001 F0004 1 1 GBSS2-LINK B 65.2 8 8 63 63 -115.8 17.4 A0001 F0004 3 133 360 GBSS2-LINK B 39.5 -10.6 -10.6 20.6 20.6 -136.5 38.9 A0001 F0004 1 1 GBSS2-LINK B 65.2 8 8 60 60 -118.8 17.4 A0001 F0004 3 133 360 GBSS2-LINK B 44 -15 -15 17.7 17.7 -139.4 38.9 A0001 F0004 1 1 GBSS2-LINK B 65.2 8 8 57 57 -121.8 17.9 A0001 F0004 3 133 360 GBSS2-LINK B 44.5 -15.5 -15.5 14.6 14.6 -142.5 38.9 CM1 CM2 3 1 TCR Link Budg 65.7 5.3 15.3 CM3 CM4 3 1 TCR Link Budg 53.8 16.2 19.2 TLM1 TLM2 1 1 TCR Link Budg 19 29 -127.8 39.8 TLM3 TLM4 1 1 TCR Link Budg 15 18 -162.8 29.9 ULP1 ULP2 2 1 TCR Link Budg 18 28 -121.8 16.2

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, D.C. 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 3070 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 4170 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 7240 8.6 0.87 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1290 4.3 0.8 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 77.1 8.6 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): 12950 12950 12950 12950 Bus (Watts): (b): (g): (l): (q): 3400 2010 2400 1600 Total (Watts): (c): (h): (m): (r): 16350 14960 15350 14550 Solar Array (Watts): (d): (i): (n): (s): 20170 17780 17800 16000 Depth of Battery (e) (j) (o) (t) Discharge (%): 74 % % 80 % % 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: 2008-06-19 10:54:53
Document Modified: 2008-06-19 10:54:53
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