Attachment Schedule S Tech Data

This document pretains to SAT-LOI-20081223-00238 for Letter of Intent on a Satellite Space Stations filing.

IBFS_SATLOI2008122300238_693508

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: NSS-9 11/15/2008 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 11/14/2006 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 8/31/2008 28 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: 10/1/2008 10/30/2008 1594 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) 3625 M 4200 M T Fixed Satellite Service 5850 M 6425 M R 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: 177 W New Skies already holds 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 this orbital location. This N/S Station-Keeping provided (Optional): application seeks authorization for a replacement d. Toward West: Degrees E/W 0.05 Degrees Tolerance: satellite in that same orbital location 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) EH S Service Area EH.gxt CAN, JAR, JON, KIR, MEX, OCE, PAQ, PLM, PTC, USA WH S Service Area WH.gxt -3dB contour GLB S Service Area GLB.gxt GLB

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) EHL R 27.1 23.1 0.12 0.39 30 N 0 EH 636 -0.9 -97 15 1 EHR R 27.1 23.1 0.12 0.39 30 N 0 EH 636 -0.9 -97 15 1 EHL T 26.8 22.8 0.12 0.39 30 N 0 EH 1.7 30 41.5 EHR T 26.8 22.8 0.12 0.39 30 N 0 EH 1.7 30 41.5 WHL R 26.4 23.4 0.12 0.39 30 N 0 WH 636 -1.6 -96 15 1 WHR R 26.4 23.4 0.12 0.39 30 N 0 WH 636 -1.6 -96 15 1 WHL T 25.9 22.9 0.12 0.39 30 N 0 WH 1.7 30 40.6 WHR T 25.9 22.9 0.12 0.39 30 N 0 WH 1.7 30 40.6 GLLU R 21 18 0.12 0.39 30 N 0 GLB 674 -7.3 -93 15 1 GLR R 21 18 0.12 0.39 30 N 0 GLB 674 -7.3 -93 15 1 GLLD T 20.6 17.6 0.12 0.39 30 N 0 GLB 1.7 30.8 35.5 GLR T 20.6 17.6 0.12 0.39 30 N 0 GLB 1.7 30.8 35.5 CMD R 13.3 12.3 0.12 0.39 30 N 0 GLB -24.1

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) EHL R C -177 EH Rx.gxt EHR R C -177 EH Rx.gxt EHL T C -177 EH Tx.gxt -154.3 -154.2 -153.5 -153.4 -152.8 EHR T C -177 EH Tx.gxt -154.3 -154.2 -153.5 -153.4 -152.8 WHL R C -177 WH Rx.gxt WHR R C -177 WH Rx.gxt WHR T C -177 WH Tx.gxt -156.8 -156.2 -155.5 -154.9 -154.3 GLLU R C -177 GLB Rx.gxt GLR R C -177 GLB Rx.gxt GLLD T C -177 GLB Tx.gxt -157.3 -157.1 -156.8 -156.6 -156.3 GLR T C -177 GLB Tx.gxt -157.3 -157.1 -156.8 -156.6 -156.3 WHL T C -177 WH Tx.gxt -156.8 -156.2 -155.5 -154.9 -154.3 CMD R C -177 Horn.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) WR01D 72000 T 3665 R C C01 123 EL01U EHLU EL01D EHLD WR02D 72000 T 3745 R C C02 123 EL02U EHLU EL02D EHLD WR03D 72000 T 3825 R C C03 123 EL03U EHLU ER03D EHLD WR04D 72000 T 3905 R C C04 123 EL04U EHLU ER04D EHLD ER01D 72000 T 3665 R C C05 123 EL01U EHLU ER01D EHRD ER02D 72000 T 3745 R C C06 123 EL02U EHLU ER02D EHRD ER03D 72000 T 3825 R C C07 123 EL03U EHLU ER03D EHRD ER04D 72000 T 3905 R C C08 123 EL04U EHLU ER04D EHRD GR05D 36000 T 3975 R C C09 123 ER01U EHRU EL01D EHLD GR06D 36000 T 4015 R C C10 123 ER02U EHRU EL02D EHLD GR07D 36000 T 4055 R C C11 123 ER03U EHRU EL03D EHLD GR08D 36000 T 4095 R C C12 123 ER04U EHRU EL04D EHLD GR09D 36000 T 4135 R C C13 123 ER01U EHRU ER01D EHRD GR10D 41000 T 4177.5 R C C14 123 ER02U EHRU ER02D EHRD WL01D 72000 T 3665 L C C15 123 ER03U EHRU ER03D EHRD WL02D 72000 T 3745 L C C16 123 ER04U EHRU ER04D EHRD WL03D 72000 T 3825 L C C17 123 EL01U EHLU WL01D WHLD WL04D 72000 T 3905 L C C18 123 EL02U EHLU WL02D WHLD EL01D 72000 T 3665 L C C19 123 EL03U EHLU WL03D WHLD EL02D 72000 T 3745 L C C20 123 EL04U EHLU WL04D WHLD EL03D 72000 T 3825 L C C21 123 EL01U EHLU WR01D WHRD EL04D 72000 T 3905 L C C22 123 EL02U EHLU WR02D WHRD GL05D 36000 T 3975 L C C23 123 EL03U EHLU WR03D WHRD GL06D 36000 T 4015 L C C24 123 EL04U EHLU WR04D WHRD GL07D 36000 T 4055 L C C25 123 ER01U EHRU WL01D WHLD GL08D 36000 T 4095 L C C26 123 ER02U EHRU WL02D WHLD GL09D 36000 T 4135 L C C27 123 ER03U EHRU WL03D WHLD GL10D 41000 T 4177.5 L C C28 123 ER04U EHRU WL04D WHLD WL01U 72000 R 5890 L C C29 123 ER01U EHRU WR01D WHRD WL02U 72000 R 5970 L C C30 123 ER02U EHRU WR02D WHRD

WL03U 72000 R 6050 L C C31 123 ER03U EHRU WR03D WHRD WL04U 72000 R 6130 L C C32 123 ER04U EHRU WR04D WHRD EL01U 72000 R 5890 L C C33 126 GR05U GLRU GL05D GLLD EL02U 72000 R 5970 L C C34 126 GR06U GLRU GL06D GLLD EL03U 72000 R 6050 L C C35 126 GR07U GLRU GL07D GLLD EL04U 72000 R 6130 L C C36 126 GR08U GLRU GL08D GLLD GL05U 36000 R 6200 L C C37 126 GR09U GLRU GL09D GLLD GL06U 36000 R 6240 L C C38 126 GR10U GLRU GL10D GLLD GL07U 36000 R 6280 L C C39 126 GL05U GLLU GR05D GLRD GL08U 36000 R 6320 L C C40 126 GL06U GLLU GR06D GLRD GL09U 36000 R 6360 L C C41 126 GL07U GLLU GR07D GLRD GL10U 41000 R 6402.5 L C C42 126 GL08U GLLU GR08D GLRD WR01U 72000 R 5890 R C C43 126 GL09U GLLU GR09D GLRD WR02U 72000 R 5970 R C C44 126 GL10U GLLU GR10D GLRD WR03U 72000 R 6050 R C C45 123 WL01U WHLU EL01D EHLD WR04U 72000 R 6130 R C C46 123 WL02U WHLU EL02D EHLD ER01U 72000 R 5890 R C C47 123 WL03U WHLU EL03D EHLD ER02U 72000 R 5970 R C C48 123 WL04U WHLU EL04D EHLD ER03U 72000 R 6050 R C C49 123 WL01U WHLU ER01D EHRD ER04U 72000 R 6130 R C C50 123 WL02U WHLU ER02D EHRD GR05U 36000 R 6200 R C C51 123 WL03U WHLU ER03D EHRD GR06U 36000 R 6240 R C C52 123 WL04U WHLU ER04D EHRD GR07U 36000 R 6280 R C C53 123 WR01U WHRU EL01D EHLD GR08U 36000 R 6320 R C C54 123 WR02U WHRU EL02D EHLD GR09U 36000 R 6360 R C C55 123 WR03U WHRU EL03D EHLD GR10U 41000 R 6402.5 R C C56 123 WR04U WHRU EL04D EHLD TM1 300 T 3951.5 R T C57 123 WR01U WHRU ER01D EHRD TM2 300 T 3952 R T C58 123 WR02U WHRU ER02D EHRD TM3 300 T 3952.5 R T C59 123 WR03U WHRU ER03D EHRD CM1 800 R 6172.1 L T C60 123 WR04U WHRU ER04D EHRD CM2 800 R 6173.7 L T C61 123 WL01U WHLU WL01D WHLD CM3 800 R 6175.3 L T C62 123 WL02U WHLU WL02D WHLD BCN 25 T 3944.75 L T C63 123 WL03U WHLU WL03D WHLD C64 123 WL04U WHLU WL04D WHLD C65 123 WL01U WHLU WR01D WHRD C66 123 WL02U WHLU WR02D WHRD C67 123 WL03U WHLU WR03D WHRD C68 123 WL04U WHLU WR04D WHRD C69 123 WR01U WHRU WL01D WHLD

C70 123 WR02U WHRU WL02D WHLD C71 123 WR03U WHRU WL03D WHLD C72 123 WR04U WHRU WL04D WHLD C73 123 WR01U WHRU WR01D WHRD C74 123 WR02U WHRU WR02D WHRD C75 123 WR03U WHRU WR03D WHRD C76 123 WR04U WHRU WR04D WHRD TM01 TM1 GLRD TM02 TM2 GLRD TM03 TM3 GLRD CM01 CM1 CMD CM02 CM2 CMD CM03 CM3 CMD

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 346KG7W 346 4 256 0.5 6 18.2 D2 461KG7W 461 4 512 0.75 9.3 21.5 D3 1M84G7W 1840 4 2048 0.75 9.3 21.5 D4 8M25G7W 8250 4 8448 0.692 6.9 19.1 D5 36M0G7W 36000 4 41470 0.692 6.9 19.1 D6 72M0G7W 72000 8 155000 0.816 12.7 24.9

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 13.2 1.5 10 24 TTC1 800KF9D 800 1 10 24 TTC2 300KF9D 300 1 0 14

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) C01 C16 D1 208 346 EH_EH_346KG 47.1 -1.8 2.2 10.3 14.3 -167.7 22.5 C01 C16 D2 110 654 EH_EH_416KG 51.2 -2.6 1.4 13.6 17.6 -165 24 C01 C16 D3 30 2400 EH_EH_1M84 53.1 -0.9 3.1 19.2 23.2 -165.8 24 C01 C16 D4 8 9000 EH_EH_8M25 47.1 10.5 14.5 24.6 28.6 -166.9 22.5 C01 C16 D6 1 EH_EH_72M0 56.3 20.7 24.7 37 41 -164 26.1 C01 C16 A1 2 36000 EH_EH_36M0F 2000 56.3 15.6 19.6 33.5 37.5 -151.9 24 C17 C32 D1 184 391 EH_WH_346K 47.1 -0.8 3.2 10.4 14.4 -167.3 22.5 C17 C32 D2 88 818 EH_WH_416K 51.2 -1.7 2.3 13.5 17.5 -164.8 24 C17 C32 D3 17 4235 EH_WH_1M84 53.1 1.6 5.6 20.7 24.7 -164 22.5 C17 C32 D4 6 12000 EH_WH_8M25 47.1 12 16 25.1 29.1 -166.1 22.5 C17 C32 D6 1 EH_WH_72M0 56.3 21.6 25.6 36 40 -164.7 26.1 C17 C32 A1 2 36000 EH_WH_36M0 2000 56.3 15.6 19.6 32.5 36.5 -152.6 24 C33 C44 D1 91 395 GL_GL_346KG 51.5 -4.1 -1.1 10.4 13.4 -168.3 24 C33 C44 D2 50 720 GL_GL_416KG 47.4 2.5 5.5 13 16 -166.7 27.1 C33 C44 D3 6 6000 GL_GL_1M84G 55.3 3.9 6.9 22.2 25.2 -163.5 22.5 C33 C44 D4 2 18000 GL_GL_8M25G 51.5 11.7 14.7 26.2 29.2 -166 22.5 C33 C44 D5 1 GL_GL_36M0G 56.7 18.7 21.7 32.5 35.5 -166.1 22.5 C33 C44 A1 1 GL_GL_36M0F 2000 56.7 18.7 21.7 32.5 35.5 -153.6 27.1 C45 C60 D1 208 346 WH_EH_346K 47.1 -3 1 10.3 14.3 -167.7 22.5 C45 C60 D2 111 649 WH_EH_416K 51.2 -1.9 2.1 13.5 17.5 -165.1 24 C45 C60 D3 30 2400 WH_EH_1M84 53.1 -0.1 3.9 19.2 23.2 -165.8 24 C45 C60 D4 8 9000 WH_EH_8M25 47.1 11.3 15.3 24.6 28.6 -166.9 22.5 C45 C60 D6 1 WH_EH_72M0 56.3 21.5 25.5 36.9 40.9 -164.1 26.1 C45 C60 A1 2 36000 WH_EH_36M0 2000 56.3 16.7 20.7 33.5 37.5 -151.9 24 C61 C76 D1 185 389 WH_WH_346K 47.1 -2 2 10.4 14.4 -167.3 22.5 C61 C76 D2 89 808 WH_WH_416K 51.2 -2.6 1.4 13.5 17.5 -164.8 24 C61 C76 D3 18 4000 WH_WH_1M84 53.1 1.9 5.9 20.3 24.3 -164.4 22.5 C61 C76 D4 6 12000 WH_WH_8M25 47.1 12.3 16.3 24.7 28.7 -166.5 22.5 C61 C76 D6 1 WH_WH_72M0 56.3 21.5 25.5 35.8 39.8 -164.9 26.1

C61 C76 A1 2 36000 WH_WH_36M0 2000 56.3 21.5 25.5 32.5 36.5 -152.6 24 TM01 TM03 TTC2 1 TELEMETRY_3 4 8 -172.9 31.7 CM01 CM03 TTC1 1 TELECOMMAN 53.4 21.6 25.6

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): #Error Remote Control (TT C) Location(s): S14a: Street Address: Newsat Networks S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Bayswater WA 6053 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): +61 894 21 466 Remote Control (TT C) Location(s): S14a: Street Address: Brewster SES Americom S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Brewster WA 98812 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): +1 509 689 1000

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 1029.1 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1249 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2278.1 12.6 0.84326 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 401.1 7.4 0.83231 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 14.96 4.1 0.70186 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): 2262.8 2262.8 2274.9 2274.9 Bus (Watts): (b): (g): (l): (q): 628.5 354.4 642.1 366 Total (Watts): (c): (h): (m): (r): 2891.3 2617.2 2917 2640.9 Solar Array (Watts): (d): (i): (n): (s): 3657 3264 3465 3156 Depth of Battery (e) (j) (o) (t) Discharge (%): 50.6 % % 72.1 % % 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? 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: 2009-02-03 14:21:55
Document Modified: 2009-02-03 14:21:55
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