Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20090807-00086 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2009080700086_730514

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: DIRECTV 12 1/31/2010 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 9/1/2004 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 10/8/2009 139 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: 10/15/2009 11/14/2009 5004 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) 18.3 G 18.8 G T Direct to Home in the Fixed Fixed Satellite Service 28.35 G 28.6 G R Fixed Satellite Service 29.25 G 29.5 G R Fixed Satellite Service 18.3 G 18.8 G T Fixed Satellite Service 19.7 G 20.2 G T Direct to Home in the Fixed Fixed Satellite Service 19.7 G 20.2 G T Fixed Satellite Service 29.5 G 30.0 G 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: 102.765 W Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be N/S Station-Keeping provided (Optional): d. Toward West: Degrees E/W 0.025 Degrees Tolerance: g. Westernmost: e. Toward East: 0.025 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) CONUS+ S CONUS + Alaska CRBC S Area around Castle Rock, CO LABC S Area around Los Angeles, CA NWUF S Area around Moxee, WA NEUF S Area around New Hampton, NH MWUF S Area around Oakdale, MN SWUF S Area around Tuscon, AZ CMD S Colorado Springs, CO CONUS S CONUS HAWAII S Hawaii

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) A1B7 T 49.1 40.1 0.062 27 N CONUS 4.3 11.1 59.5 A1B8 T 48.9 39.9 0.062 27 N CONUS 4.2 11.5 59.5 A1B9 T 49.1 40.1 0.062 27 N CONUS 4.3 11.1 59.5 A1BA T 48.9 39.9 0.062 27 N CONUS 4.2 11.4 59.5 A1BB T 48.8 39.8 0.062 27 N CONUS 4.1 11.8 59.5 A1BC T 48.5 39.5 0.062 27 N CONUS 3.8 12.6 59.5 A2B1 T 48.5 39.5 0.062 27 N CONUS 3.7 12.7 59.5 A2B2 T 48.4 39.4 0.062 27 N CONUS 3.7 12.8 59.5 A2B3 T 48.4 39.4 0.062 27 N CONUS 3.7 12.8 59.5 A2B4 T 48.5 39.5 0.062 27 N CONUS 3.7 12.7 59.5 A2B5 T 48.5 39.5 0.062 27 N CONUS 3.7 12.7 59.5 A2B6 T 48.4 39.4 0.062 27 N CONUS 3.7 12.8 59.5 A2B7 T 48.5 39.5 0.062 27 N CONUS 3.8 12.5 59.5 A2B8 T 48.5 39.5 0.062 27 N CONUS 3.8 12.5 59.5 A2B9 T 49 40 0.062 27 N CONUS 4.3 11.2 59.5 A2BA T 48.8 39.8 0.062 27 N CONUS 4.1 11.6 59.5 A2BB T 48.9 39.9 0.062 27 N CONUS 4.1 11.6 59.5 A2BC T 48.6 39.6 0.062 27 N CONUS 3.9 12.2 59.5 A2BD T 48.5 39.5 0.062 27 N CONUS 3.8 12.6 59.5 A3B1 T 48.5 39.5 0.062 27 N CONUS 3.8 12.5 59.5 A3B2 T 49.1 40.1 0.062 27 N CONUS 4.3 11 59.5 A3B3 T 48.8 39.8 0.062 27 N CONUS 4 11.9 59.5 A3B4 T 48.7 39.7 0.062 27 N CONUS 3.9 12.1 59.5 A3B5 T 48.7 39.7 0.062 27 N CONUS 4 11.9 59.5 A3B6 T 49.3 40.3 0.062 27 N CONUS 4.6 10.5 59.5 A3B7 T 49.2 40.2 0.062 27 N CONUS 4.5 10.7 59.5 A3B8 T 49.1 40.1 0.062 27 N CONUS 4.3 11.1 59.5 A3B9 T 49.1 40.1 0.062 27 N CONUS 4.4 10.9 59.5 A3BA T 48.9 39.9 0.062 27 N CONUS 4.2 11.5 59.5

A3BB T 47.6 38.6 0.062 27 N HAWAII 2.9 15.5 59.5 A4B1 T 48.7 39.7 0.062 27 N CONUS 3.9 12.1 59.5 A4B2 T 49.1 40.1 0.062 27 N CONUS 4.4 11 59.5 A4B3 T 48.7 39.7 0.062 27 N CONUS 4 11.9 59.5 A4B4 T 48.9 39.8 0.062 27 N CONUS 4.2 11.5 59.5 A4B5 T 48.9 39.9 0.062 27 N CONUS 4.1 11.6 59.5 A4B6 T 48.9 39.9 0.062 27 N CONUS 4.2 11.4 59.5 A4B7 T 49.4 40.4 0.062 27 N CONUS 4.7 10.3 59.5 A4B8 T 49.2 40.2 0.062 27 N CONUS 4.5 10.7 59.5 A4B9 T 49.4 40.4 0.062 27 N CONUS 4.7 10.1 59.5 A4BA T 49.1 40.1 0.062 27 N CONUS 4.4 10.8 59.5 A4BB T 49 40 0.062 27 N CONUS 4.3 11.1 59.5 A4BC T 48.8 39.8 0.062 27 N CONUS 4.1 11.6 59.5 A4BD T 48.6 39.6 0.062 27 N CONUS 3.9 12.2 59.5 TLM T 24 22 0.1 27 N CONUS 2 14.4 35.6 UL1 R 50.8 48.8 0.1 27 N LABC 1000 20.8 -105 19 1 UL2 R 51.2 49.2 0.1 27 N CRBC 1000 21.2 -105 19 1 DL1 T 36.3 28.3 0.1 27 N CONUS+ 1 2.2 58.3 CMD R 38.5 37.5 0.1 27 N CMD 17783 -4 UL3 R 51 49 0.1 27 N SWUF 1000 21 -105 19 1 UL4 R 50.8 48.8 0.1 27 N NWUF 1000 20.8 -105 19 1 UL5 R 49.7 47.7 0.1 27 N NEUF 1000 19.7 -105 19 1 UL6 R 50.9 48.9 0.1 27 N MWUF 1000 20.9 -105 19 1 A1B1 T 48.5 39.5 0.062 27 N CONUS 3.8 12.5 59.5 A1B2 T 48.8 39.8 0.062 27 N CONUS 4.1 11.7 59.5 A1B3 T 48.6 39.6 0.062 27 N CONUS 3.9 12.2 59.5 A1B4 T 49.1 40.1 0.062 27 N CONUS 4.4 10.9 59.5 A1B5 T 48.6 39.6 0.062 27 N CONUS 3.9 12.2 59.5 A1B6 T 48.8 39.8 0.062 27 N CONUS 4 11.9 59.5

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)

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) TC09 36000 T 19890 R C NAT9 114 RC09 UL1 TC09 DL1 TC10 36000 T 19890 L C NAT10 114 RC10 UL1 TC10 DL1 TC11 36000 T 19930 R C NAT11 114 RC11 UL1 TC11 DL1 TC12 36000 T 19930 L C NAT12 114 RC12 UL1 TC12 DL1 TC13 36000 T 19970 R C NAT13 114 RC13 UL1 TC13 DL1 TC14 36000 T 19970 L C NAT14 114 RC14 UL1 TC14 DL1 TC15 36000 T 20010 R C NAT15 114 RC15 UL1 TC15 DL1 TC16 36000 T 20010 L C NAT16 114 RC16 UL1 TC16 DL1 TC17 36000 T 20050 R C NAT17 114 RC17 UL1 TC17 DL1 TC18 36000 T 20050 L C NAT18 114 RC18 UL1 TC18 DL1 TC19 36000 T 20090 R C NAT19 114 RC19 UL1 TC19 DL1 TC20 36000 T 20090 L C NAT20 114 RC20 UL1 TC20 DL1 TC21 36000 T 20130 R C NAT21 114 RC21 UL1 TC21 DL1 TC22 36000 T 20130 L C NAT22 114 RC22 UL1 TC22 DL1 TC23 36000 T 20170 R C NAT23 114 RC23 UL1 TC23 DL1 TC24 36000 T 20170 L C NAT24 114 RC24 UL1 TC24 DL1 TS15 36000 T 18604 R C CMD1 CMD1 CMD TS16 36000 T 18604 L C CMD2 CMD2 CMD TS17 36000 T 18648 R C SP11 102 RS16L UL5 TS16 A1B1 TS18 36000 T 18648 L C SP12 102 RS19L UL5 TS19 A1B1 TS19 36000 T 18692 R C SP13 102 RS20L UL5 TS20 A1B1 TS20 36000 T 18692 L C SP21 102 RS16U UL3 TS16 A1B2 TS21 36000 T 18732 R C SP22 102 RS19U UL5 TS19 A1B2 TS22 36000 T 18732 L C SP23 102 RS20U UL3 TS20 A1B2 TS23 36000 T 18776 R C SP31 102 RS16U UL5 TS16 A1B3 TS24 36000 T 18776 L C SP32 102 RS19U UL6 TS19 A1B3 RS21 36000 R 29437 R C SP33 102 RS20U UL5 TS20 A1B3 RS22 36000 R 29437 L C SP41 102 RS16L UL6 TS16 A1B4 RS23 36000 R 29481 R C SP42 102 RS19L UL6 TS19 A1B4 RS24 36000 R 29481 L C SP43 102 RS20L UL6 TS20 A1B4

RC09 36000 R 29690 R C SP51 102 RS16L UL3 TS16 A1B5 RC10 36000 R 29690 L C SP52 102 RS19U UL2 TS19 A1B5 RC11 36000 R 29730 R C SP53 102 RS20L UL3 TS20 A1B5 RC12 36000 R 29730 L C SP61 102 RS16U UL2 TS16 A1B6 RC13 36000 R 29770 R C SP62 102 RS19L UL3 TS19 A1B6 RC14 36000 R 29770 L C SP71 102 RS16U UL6 TS16 A1B7 RC15 36000 R 29810 R C SP72 102 RS19U UL4 TS19 A1B7 RC16 36000 R 29810 L C SP73 102 RS20U UL6 TS20 A1B7 RC17 36000 R 29850 R C SP81 102 RS16U UL3 TS16 A1B8 RC18 36000 R 29850 L C SP82 102 RS19U UL5 TS19 A1B8 RC19 36000 R 29890 R C SP83 102 RS20U UL3 TS20 A1B8 RC20 36000 R 29890 L C TLM1 TLM1 TLM RC21 36000 R 29930 R C TLM2 TLM2 TLM RC22 36000 R 29930 L C SP91 102 RS16L UL2 TS16 A1B9 RC23 36000 R 29970 R C SP92 102 RS19L UL2 TS19 A1B9 RC24 36000 R 29970 L C SP93 102 RS20L UL2 TS20 A1B9 CMD1 1300 R 29255 L T SP101 102 RS16U UL4 TS16 A1BA CMD2 1300 R 29495 L T SP102 102 RS19U UL3 TS19 A1BA TLM1 106 T 18302.25 R T SP103 102 RS20U UL4 TS20 A1BA TLM1B 106 T 18302.25 L T SP111 102 RS16 UL1 TS16 A1BB TLM2 106 T 18302.75 L T SP112 102 RS19 UL1 TS19 A1BB RS15L 36000 R 28389 R C SP131 102 RS15L UL5 TS15 A2B1 RS16L 36000 R 28389 L C SP132 102 RS23L UL5 TS23 A2B1 RS17L 36000 R 28433 R C SP133 102 RS24L UL5 TS24 A2B1 RS18L 36000 R 28433 L C SP141 102 RS15U UL5 TS15 A2B2 RS19L 36000 R 28477 R C SP142 102 RS23U UL5 TS23 A2B2 RS20L 36000 R 28477 L C SP143 102 RS24U UL5 TS24 A2B2 RS21L 36000 R 28517 R C SP161 102 RS15L UL6 TS15 A2B4 RS22L 36000 R 28517 L C SP162 102 RS23L UL6 TS23 A2B4 RS23L 36000 R 28561 R C SP163 102 RS24L UL6 TS24 A2B4 RS24L 36000 R 28561 L C SP171 102 RS15U UL6 TS15 A2B5 RS15U 36000 R 29285 R C SP172 102 RS23U UL6 TS23 A2B5 RS16U 36000 R 29285 L C SP173 102 RS24L UL3 TS24 A2B5 RS17U 36000 R 29329 R C SP181 102 RS15U UL2 TS15 A2B6 RS18U 36000 R 29329 L C SP182 102 RS23U UL2 TS23 A2B6 RS19U 36000 R 29373 R C SP183 102 RS24U UL2 TS24 A2B6 RS20U 36000 R 29373 L C SP201 102 RS15L UL3 TS15 A2B8 RS21U 36000 R 29413 R C SP202 102 RS23L UL3 TS23 A2B8 RS22U 36000 R 29413 L C SP203 102 RS24U UL6 TS24 A2B8

RS23U 36000 R 29457 R C SP211 102 RS15U UL4 TS15 A2B9 RS24U 36000 R 29457 L C SP212 102 RS23U UL4 TS23 A2B9 RS15 36000 R 29309 R C SP213 102 RS24L UL2 TS24 A2B9 RS16 36000 R 29309 L C SP221 102 RS15L UL2 TS15 A2BA RS17 36000 R 29353 R C SP222 102 RS23L UL2 TS23 A2BA RS18 36000 R 29353 L C SP223 102 RS24 UL1 TS24 A2BA RS19 36000 R 29397 R C SP231 102 RS15U UL3 TS15 A2BB RS20 36000 R 29397 L C SP232 102 RS23U UL3 TS23 A2BB SP233 102 RS24U UL3 TS24 A2BB SP241 102 RS15L UL4 TS15 A2BC SP242 102 RS23L UL4 TS23 A2BC SP251 102 RS15 UL1 TS15 A2BD SP252 102 RS23 UL1 TS23 A2BD SP253 102 RS24U UL4 TS24 A2BD SP261 102 RS17L UL5 TS17 A3B1 SP262 102 RS18U UL5 TS18 A3B1 SP271 102 RS17U UL5 TS17 A3B2 SP272 102 RS18L UL5 TS18 A3B2 SP281 102 RS17L UL6 TS17 A3B3 SP282 102 RS18L UL6 TS18 A3B3 SP291 102 RS17L UL2 TS17 A3B4 SP292 102 RS18L UL2 TS18 A3B4 SP301 102 RS17U UL6 TS17 A3B5 SP302 102 RS18U UL6 TS18 A3B5 SP311 102 RS17U UL2 TS17 A3B6 SP312 102 RS18U UL2 TS18 A3B6 SP321 102 RS17U UL3 TS17 A3B7 SP322 102 RS18U UL3 TS18 A3B7 SP331 102 RS17L UL4 TS17 A3B8 SP332 102 RS18L UL4 TS18 A3B8 SP341 102 RS17 UL1 TS17 A3B9 SP342 102 RS18 UL1 TS18 A3B9 SP351 102 RS17U UL4 TS17 A3BA SP352 102 RS18U UL4 TS18 A3BA SP371 102 RS21U UL5 TS21 A4B1 SP372 102 RS22L UL5 TS22 A4B1 SP381 102 RS21L UL5 TS21 A4B2 SP382 102 RS22U UL5 TS22 A4B2 SP391 102 RS21L UL6 TS21 A4B3

SP392 102 RS22L UL6 TS22 A4B3 SP401 102 RS21L UL2 TS21 A4B4 SP402 102 RS22L UL2 TS22 A4B4 SP411 102 RS21U UL6 TS21 A4B5 SP412 102 RS22U UL6 TS22 A4B5 SP421 102 RS21U UL2 TS21 A4B6 SP422 102 RS22U UL2 TS22 A4B6 SP431 102 RS21U UL3 TS21 A4B7 SP432 102 RS22U UL3 TS22 A4B7 SP441 102 RS21L UL4 TS21 A4B8 SP442 102 RS22L UL4 TS22 A4B8 SP451 102 RS21L UL3 TS21 A4B9 SP452 102 RS22L UL3 TS22 A4B9 SP461 102 RS21L UL3 TS21 A4BA SP462 102 RS22L UL3 TS22 A4BA SP471 102 RS21 UL1 TS21 A4BB SP472 102 RS22 UL1 TS22 A4BB SP481 102 RS21U UL4 TS21 A4BC SP482 102 RS22U UL4 TS22 A4BC SP63 102 RS20U UL2 TS20 A1B6 SP113 102 RS20 UL1 TS20 A1BB SP121 102 RS16L UL4 TS16 A1BC SP122 102 RS19L UL4 TS19 A1BC SP123 102 RS20L UL4 TS20 A1BC SP151 102 RS15U UL5 TS15 A2B3 SP152 102 RS23U UL5 TS23 A2B3 SP153 102 RS24U UL5 TS24 A2B3 SP191 102 RS15U UL6 TS15 A2B7 SP192 102 RS23U UL6 TS23 A2B7 SP193 102 RS24L UL3 TS24 A2B7 SP243 102 RS24L UL4 TS24 A2BC SP361 102 RS17L UL3 TS17 A3BB SP362 102 RS18L UL3 TS18 A3BB SP491 102 RS21U UL4 TS21 A4BD SP492 102 RS22U UL4 TS22 A4BD TLM1B TLM1B TLM

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) M2 36M0G7W 36000 4 34.8 0.58 3.8 16 M3 36M0G7W 36000 4 38720 0.6453 4.7 16.9

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) CMD 1M30F9D 1300 1 9.5 21.7 TLM 106KG9D 106 1 5.5 17.7

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) NAT9 NAT24 M3 1 66.3 7.6 13.6 52.3 58.3 -119.2 18.4 SP11 SP492 M2 1 66.3 7.6 13.6 53.5 59.5 -118 18.4 CMD1 CMD2 CMD 1 66.3 23.7 23.7 90 90 TLM1 TLM2 TLM 1 24 -5.9 11.6 18.1 35.6 -126.4 31

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: 1600 Forbes Way S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Long Beach Los Angeles CA 90810 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 310 525 5590

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 3556 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2440 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5996 47.9 0.6 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 266 8.2 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 77 7.3 0.51 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): 14330 14330 14330 14330 Bus (Watts): (b): (g): (l): (q): 1800 700 1800 700 Total (Watts): (c): (h): (m): (r): 16130 15030 16130 15030 Solar Array (Watts): (d): (i): (n): (s): 20050 17900 16900 15700 Depth of Battery (e) (j) (o) (t) Discharge (%): 79.5 % 0 % 79.5 % 0 % 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: 2009-08-11 13:40:19
Document Modified: 2009-08-11 13:40:19
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