Attachment Sched S Tech Report

This document pretains to SES-LIC-20100723-00952 for License on a Satellite Earth Station filing.

IBFS_SESLIC2010072300952_832612

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: O3B 9/30/2012 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 12/15/2008 10 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 3/1/2012 20 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: 3/31/2012 12/31/2012 4320 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) 27600 M 28400 M R Fixed Satellite Service 19290 M 19300 M T Space Operations Service 29085 M 29100 M R Space Operations Service 17800 M 18600 M T Fixed Satellite Service 18800 M 19290 M T Fixed Satellite Service 28600 M 29085 M T Fixed Satellite Service S3. ORBITAL INFORMATION FOR GEOSTATIONARY SATELLITES ONLY:

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: 8 S4c. Celestial Reference Body (Earth, Sun, Moon, etc.): E S4b. Total Number of Orbital Planes in Network or System: 1 S4d. Orbit Epoch Date: 1/1/2010 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 1 8 0 17280 8062 8062 0 0 0 360 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) 1 1 0 1 2 45 1 3 90 1 4 135 1 5 180 1 6 225 1 7 270 1 8 315

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) G1 S Haleiwa, HI U S Visible Earth down to a minimum elevation angle of 3 degrees

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) GT1 T 33.1 29.1 0.6 0.5 18.5 N G1 1.5 45.9 49.7 GT2 T 33.1 29.1 0.6 0.5 18.5 N G1 1.5 45.9 49.7 GR1 R 34.5 31.5 0.6 0.5 18.5 N G1 1000 4 -98 14 0.5 GR2 R 34.5 31.5 0.6 0.5 18.5 N G1 1000 4 -98 14 0.5 UT1 T 33.1 29.1 0.6 0.5 18.5 N U 1.5 45.9 49.7 UT2 T 33.1 29.1 0.6 0.5 18.5 N U 1.5 45.9 49.7 UT3 T 33.1 29.1 0.6 0.5 18.5 N U 1.5 45.9 49.7 UT4 T 33.1 29.1 0.6 0.5 18.5 N U 1.5 45.9 49.7 UT5 T 33.1 29.1 0.6 0.5 18.5 N U 1.5 45.9 49.7 UT6 T 33.1 29.1 0.6 0.5 18.5 N U 1.5 45.9 49.7 UT7 T 33.1 29.1 0.6 0.5 18.5 N U 1.5 45.9 49.7 UT8 T 33.1 29.1 0.6 0.5 18.5 N U 1.5 45.9 49.7 UT9 T 33.1 29.1 0.6 0.5 18.5 N U 1.5 45.9 49.7 UT10 T 33.1 29.1 0.6 0.5 18.5 N U 1.5 45.9 49.7 UR1 R 34.5 31.5 0.6 0.5 18.5 N U 1000 4 -101 14 0.5 UR2 R 34.5 31.5 0.6 0.5 18.5 N U 1000 4 -101 14 0.5 UR3 R 34.5 31.5 0.6 0.5 18.5 N U 1000 4 -101 14 0.5 UR4 R 34.5 31.5 0.6 0.5 18.5 N U 1000 4 -101 14 0.5 UR5 R 34.5 31.5 0.6 0.5 18.5 N U 1000 4 -101 14 0.5 UR6 R 34.5 31.5 0.6 0.5 18.5 N U 1000 4 -101 14 0.5 UR7 R 34.5 31.5 0.6 0.5 18.5 N U 1000 4 -101 14 0.5 UR8 R 34.5 31.5 0.6 0.5 18.5 N U 1000 4 -101 14 0.5 UR9 R 34.5 31.5 0.6 0.5 18.5 N U 1000 4 -101 14 0.5 UR10 R 34.5 31.5 0.6 0.5 18.5 N U 1000 4 -101 14 0.5 CMD R 8 6 0.6 0.5 20 N U 1000 -20 -92 TLM T 8 6 0.6 0.5 20 N U 1 0.52 5.2 TLM T 8 1 0.6 0.5 20 N U 4.5 17.78 20.5

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) GT1 T C Tx_Gatway_Hawaii_158E.pdf -119.19 -118.82 -118.46 -118.11 -117.77 GR1 R C Rx_Gatway_Hawaii_158E.pdf GR2 R C Rx_Gatway_Hawaii_158E.pdf UT1 T C Tx_User_Suva_158E.pdf -119.19 -118.82 -118.46 -118.11 -117.77 UT2 T C Tx_User_Suva_158E.pdf -119.19 -118.82 -118.46 -118.11 -117.77 UT3 T C Tx_User_Suva_158E.pdf -119.19 -118.82 -118.46 -118.11 -117.77 UT4 T C Tx_User_Suva_158E.pdf -119.19 -118.82 -118.46 -118.11 -117.77 UT5 T C Tx_User_Suva_158E.pdf -119.19 -118.82 -118.46 -118.11 -117.77 UT6 T C Tx_User_Suva_158E.pdf -119.19 -118.82 -118.46 -118.11 -117.77 UT7 T C Tx_User_Suva_158E.pdf -119.19 -118.82 -118.46 -118.11 -117.77 UT8 T C Tx_User_Suva_158E.pdf -119.19 -118.82 -118.46 -118.11 -117.77 UT9 T C Tx_User_Suva_158E.pdf -119.19 -118.82 -118.46 -118.11 -117.77 UT10 T C Tx_User_Suva_158E.pdf -119.19 -118.82 -118.46 -118.11 -117.77 UR1 R C Rx_User_Suva_158E.pdf UR2 R C Rx_User_Suva_158E.pdf UR3 R C Rx_User_Suva_158E.pdf UR4 R C Rx_User_Suva_158E.pdf UR5 R C Rx_User_Suva_158E.pdf UR6 R C Rx_User_Suva_158E.pdf UR7 R C Rx_User_Suva_158E.pdf UR8 R C Rx_User_Suva_158E.pdf UR9 R C Rx_User_Suva_158E.pdf GT2 T C Tx_Gatway_Hawaii_158E.pdf -119.19 -118.82 -118.46 -118.11 -117.77 UR10 R C Rx_User_Suva_158E.pdf CMD R C CMD.pdf TLM T C TLMN.pdf -147.7 -147.3 -146.9 -146.6 -146.2 TLM T C TLMS.pdf -132.4 -132 -131.6 -131.3 -130.9

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) R1L 216000 R 27760 L C F1 105 R1R GR1 T1L UT1 R1R 216000 R 27760 R C F2 105 R2R GR1 T2L UT2 R2L 216000 R 28020 L C F3 105 R3R GR1 T3L UT3 R2R 216000 R 28020 R C F4 105 R4R GR1 T4L UT4 R3L 216000 R 28280 L C F5 105 R5R GR1 T5L UT5 R3R 216000 R 28280 R C F6 105 R1L GR2 T1R UT6 R4L 216000 R 28709 L C F7 105 R2L GR2 T2R UT7 R4R 216000 R 28709 R C F8 105 R3L GR2 T3R UT8 R5L 216000 R 28963 L C F9 105 R4L GR2 T4R UT9 R5R 216000 R 28963 R C F10 105 R5L GR2 T5R UT10 T1L 216000 T 17960 L C R1 108 R1L UR1 T1R GT1 T1R 216000 T 17960 R C R2 108 R2L UR2 T2R GT1 T2L 216000 T 18220 L C R3 108 R3L UR3 T3R GT1 T2R 216000 T 18220 R C R4 108 R4L UR4 T4R GT1 T3L 216000 T 18480 L C R5 108 R5L UR5 T5R GT1 T3R 216000 T 18480 R C R6 108 R1R UR6 T1L GT2 T4L 216000 T 18909 L C R7 108 R2R UR7 T2L GT2 T4R 216000 T 18909 R C R8 108 R3R UR8 T3L GT2 T5L 216000 T 19163 L C R9 108 R4R UR9 T4L GT2 T5R 216000 T 19163 R C R10 108 R5R UR10 T5L GT2 TM1 1000 T 19296.6 R T TC TC1 CMD TM2 1000 T 19296.8 R T TMN1 TM1 TLMN TM3 1000 T 19297 R T TMN2 TM2 TLMN TM4 1000 T 19297.2 R T TMN3 TM3 TLMN TM5 1000 T 19297.4 R T TMN4 TM4 TLMN TM6 1000 T 19297.6 R T TMN5 TM5 TLMN TM7 1000 T 19297.8 R T TMN6 TM6 TLMN TM8 1000 T 19298 R T TMN7 TM7 TLMN TM9 1000 T 19298.2 R T TMN8 TM8 TLMN TM10 1000 T 19298.4 R T TMN9 TM9 TLMN

TM11 1000 T 19298.6 R T TMN10 TM10 TLMN TM12 1000 T 19298.8 R T TMN11 TM11 TLMN TM13 1000 T 19299 R T TMN12 TM12 TLMN TM14 1000 T 19299.2 R T TMN13 TM13 TLMN TM15 1000 T 19299.4 R T TMN14 TM14 TLMN TM16 1000 T 19299.6 R T TMN15 TM15 TLMN TC1 1200 R 29088.5 L T TMN16 TM16 TLMN TMS1 1000 T 19296.6 L T TMS1 TMS1 TLMS TMS2 1000 T 19296.8 L T TMS2 TMS2 TLMS TMS3 1000 T 19297 L T TMS3 TMS3 TLMS TMS4 1000 T 19297.2 L T TMS4 TMS4 TLMS TMS5 1000 T 19297.4 L T TMS5 TMS5 TLMS TMS6 1000 T 19297.6 L T TMS6 TMS6 TLMS TMS7 1000 T 19297.8 L T TMS7 TMS7 TLMS TMS8 1000 T 19298 L T TMS8 TMS8 TLMS TMS9 1000 T 19298.2 L T TMS9 TMS9 TLMS TMS10 1000 T 19298.4 L T TMS10 TMS10 TLMS TMS11 1000 T 19298.6 L T TMS11 TMS11 TLMS TMS12 1000 T 19298.8 L T TMS12 TMS12 TLMS TMS13 1000 T 19299 L T TMS13 TMS13 TLMS TMS14 1000 T 19299.2 L T TMS14 TMS14 TLMS TMS15 1000 T 19299.4 L T TMS15 TMS15 TLMS TMS16 1000 T 19299.6 L T TMS16 TMS16 TLMS F11 105 R4R UR6 T4L UT4 F12 105 R5R UR6 T5L UT5 F13 105 R2L UR6 T2R UT7 F14 105 R3R UR9 T3L UT3 F15 105 R2L UR9 T2R UT7 F16 105 R3L UR1 T3R UT8 F17 105 R4R UR3 T4L UT4 R11 108 R4L UR4 T4R UT6 R12 108 R5L UR5 T5R UT6 R13 108 R2R UR7 T2L UT6 R14 108 R3L UR3 T3R UT9 R15 108 R2R UR7 T2L UT9 R16 108 R3R UR8 T3L UT1 R17 108 R4L UR4 T4R UT3 F18 105 R1L UR1 T1L UT1 F19 105 R3L UR3 T3L UT3

F20 105 R5L UR5 T5L UT5 F21 105 R3R UR8 T3R UT8

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 216MX7D 216000 32 725506 0.833 18.1 30.3 D2 216MX7D 216000 16 520901 0.75 13.6 25.8 D3 216MX7D 216000 8 348127 0.667 8.8 21 D4 216MX7D 216000 4 232147 0.667 5.3 17.5 D5 216MX7D 216000 4 86071 0.25 -1.2 11 D6 40M0X7D 40000 16 134352 0.833 18.1 30.3 D7 40M0X7D 40000 8 96463 0.75 13.6 25.8 D8 40M0X7D 40000 4 64467 0.667 8.8 21 D9 40M0X7D 40000 8 42990 0.667 5.3 17.5 D10 40M0X7D 40000 4 15939 0.25 -1.2 11 D11 307KX7D 1000 32 859 0.833 18.1 30.3 D12 307KX7D 1000 16 617 0.75 13.6 25.8 D13 307KX7D 1000 8 412 0.667 8.8 21 CMD2 500KG2D 1200 2 10 1 10 22.2 TLM2 300KG1D 1000 2 8.192 1 10 22.2 D14 307KX7D 40000 4 275 0.667 5.3 17.5 D15 307KX7D 40000 4 102 0.25 -1.2 11

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)

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) F1 F21 D3 1 Link_1.doc 65 13.5 22 40.5 47.7 -125 32 R1 R17 D3 1 Link_2.doc 59 18.1 21.1 31.8 36.9 -127 37 F1 F21 D1 1 Link_3.doc 65 12.5 22 40.6 47.7 -125 32 R1 R17 D1 1 Link_4.doc 59 17.1 21.1 32.8 37.9 -127 37 F1 F21 D5 1 Link_5.doc 65 12.5 22 40.5 47.7 -125 32 R1 R17 D5 1 Link_6.doc 59 19.1 22.1 32.8 37.9 -127 37 F1 F21 D4 1 Link_7.doc 65 11.5 22 40.6 47.7 -125 32 R1 R17 D4 1 Link_8.doc 59 19.1 22.1 32.3 37.9 -127 37 F1 F21 D2 1 Link_9.doc 65 12.5 22 37.9 47.7 -125 32 R1 R17 D2 1 Link_10.doc 59 19.1 22.1 32.8 37.9 -127 37 F4 F5 D7 1 Link_11.doc 65 12.5 22 37.4 47.7 -118 32 R4 R5 D7 1 Link_12.doc 59 19.6 22.6 32.8 37.9 -127 37 F9 F10 D6 1 Link_13.doc 65 12.5 22 40.4 47.7 -118 32 R9 R10 D6 1 Link_14.doc 59 18.1 22.1 32.8 37.9 -127 37 F4 F5 D10 1 Link_15.doc 65 12.5 22 40.3 47.7 -118 26 F9 F10 D8 1 Link_16.doc 65 12.5 22 40.5 47.7 -118 26 F1 F21 D15 703 Link_17.doc 65 -16 -13 6.4 19.2 -125 26 R1 R17 D15 703 Link_18.doc 51 4.4 9.4 -1.7 2.3 -127 37 F1 F21 D13 703 Link_19.doc 65 -16 -13 9.5 19.2 -125 26 R1 R17 D13 703 Link_20.doc 51 4.4 9.4 -1.7 2.3 -127 37 R4 R5 D10 1 Link_21.doc 51 1.6 4.6 32.8 37.9 -127 37 R9 R10 D8 1 Link_22.doc 51 12.4 15.4 32.8 37.9 -127 37 TC TC CMD2 1 Link_TLC.doc 65 17.2 20.2 TMN1 TMN16 TLM2 1 Link_TLMN.doc -1 5.2 -143 37 TMS1 TMS16 TLM2 1 Link_TLMS.doc 6.6 20.5 -128 37

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: 58-350 Kamehameha Hwy S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Haleiwa Honolulu HI 96712 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): (808) 638-0389

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 557 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 143 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 700 3.19 0.993 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 143 7.72 0.866 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 7 0.8 0.86 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): 1140 1140 727 727 Bus (Watts): (b): (g): (l): (q): 220 220 213 213 Total (Watts): (c): (h): (m): (r): 1360 1360 940 940 Solar Array (Watts): (d): (i): (n): (s): 1529 1697 1036 1159 Depth of Battery (e) (j) (o) (t) Discharge (%): 32.9 % 15 % 19.7 % 9 % 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 X 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: 2010-08-02 19:14:15
Document Modified: 2010-08-02 19:14:15
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