Attachment Schedule S Tech Data

This document pretains to SAT-PPL-20060329-00030 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2006032900030_491743

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: SATMEX 6 7/1/2006 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 1/15/2001 15.2 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 7/25/2003 60 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: 5/17/2006 5/17/2006 2160 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 14000 M 14500 M R Fixed Satellite Service 11700 M 12200 M T Fixed Satellite Service 3700 M 4200 M T Direct to Home in the Fixed Fixed Satellite Service 11700 M 12200 M T Direct to Home in the Fixed 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: 113 W The orbital location is consistent with the Trilateral Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Agreement reached between Canada, Mexico and the N/S Station-Keeping provided (Optional): United States of America in 1988. d. Toward West: Degrees E/W 0.05 Degrees Tolerance: 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) SA1 S -6 dB contour of beam CCUH SA2 S -6 dB contour of beam CCUV SA3 S -6 dB contour of beam CCDH SA4 S -6 dB contour of beam CCDV SA5 S -6 dB contour of beam CHUH SA6 S -6 dB contour of beam CHUV SA7 S -6 dB contour of beam CHDH SA8 S -6 dB contour of beam CHDV SA9 S -6 dB contour of beam CSUH SA10 S -6 dB contour of beam CSUV SA11 S -6 dB contour of beam CSDH SA12 S -6 dB contour of beam CSDV SA13 S -6 dB contour of beam KNUH SA14 S -6 dB contour of beam KNUV SA15 S -6 dB contour of beam KNDH SA16 S -6 dB contour of beam KNDV SA17 S -6 dB contour of beam KHUH SA18 S -6 dB contour of beam KHUV SA19 S -6 dB contour of beam KHDH SA20 S -6 dB contour of beam KHDV SA21 S Visible Earth

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) CCU R 30.6 24.6 0.13 0 27 N 0 SA1 457 4 -98 31 1 CCU R 30.6 24.6 0.13 0 27 N 90 SA2 457 4 -98 31 1 CCD T 30.3 24.3 0.13 0 27 N 0 SA3 1.7 31.6 45.3 CCD T 30.3 24.3 0.13 0 27 N 90 SA4 1.5 33.1 45.5 CHU R 28.5 22.5 0.13 0 27 N 0 SA5 479 1.7 -98 31 1 CHU R 27.6 21.6 0.13 0 27 N 90 SA6 468 0.9 -98 31 1 CHD T 27.9 21.9 0.13 0 27 N 0 SA7 1.5 33.1 43.1 CHD T 25.9 19.9 0.13 0 27 N 90 SA8 1.5 33.9 41.2 CSU R 31.6 25.6 0.13 0 30 N 0 SA9 380 5.8 -98 31 1 CSU R 31.6 25.6 0.13 0 30 N 90 SA10 380 5.8 -98 31 1 CSD T 31.1 25.1 0.13 0 30 N 0 SA11 1.6 24.5 45 CSD T 31.1 25.1 0.13 0 30 N 90 SA12 1.6 24.5 45 KNU R 34.4 28.4 0.13 0 30 N 0 SA13 692 6 -96 36 1 KNU R 34.4 28.4 0.13 0 30 N 90 SA14 692 6 -96 36 1 KND T 33.3 27.3 0.13 0 30 N 0 SA15 2.7 79.4 52.3 KND T 33.3 27.3 0.13 0 30 N 90 SA16 2.4 85.1 52.6 KHU R 31 25 0.13 0 30 N 0 SA17 603 3.2 -96 36 1 KHU R 31 25 0.13 0 30 N 90 SA18 603 3.2 -96 36 1 KHD T 30 24 0.13 0 30 N 0 SA19 2.9 129 51.1 KHD T 30 24 0.13 0 30 N 90 SA20 2.6 138 51.4 OMNI R 2 0 0.13 0 30 N SA21 9600 -37.8

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) CCU R C -113 CCUH.gxt CCU R C -113 CCUV.gxt CCD T C -113 CCDH.gxt -152.3 -152.1 -151.7 -151.2 -150.3 CCD T C -113 CCDV.gxt -152.8 -152.5 -152.2 -151.6 -150.6 CHU R C -113 CHUH.gxt CHU R C -113 CHUV.gxt CHD T C -113 CHDH.gxt -152 -151.7 -151.3 -150.8 -150.4 CHD T C -113 CHDV.gxt -152 -151.7 -151.5 -151.1 -150.7 CSU R C -113 CSUH.gxt CSU R C -113 CSUV.gxt CSD T C -113 CSDH.gxt -152 -151.5 -150.8 -150 -149.1 CSD T C -113 CSDV.gxt -152 -151.4 -150.8 -150 -149.1 KNU R C -113 KNUH.gxt KNU R C -113 KNUV.gxt KND T C -113 KNDH.gxt KND T C -113 KNDV.gxt KHU R C -113 KHUH.gxt KHU R C -113 KHUV.gxt KHD T C -113 KHDH.gxt KHD T C -113 KHDV.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) CU001 36000 R 5945 H C K0027 131 KU018 KHUH KD018 KHDV CU003 36000 R 5985 H C K0028 131 KU020 KHUH KD020 KHDV CU005 36000 R 6025 H C K0029 131 KU022 KHUH KD022 KHDV CU007 36000 R 6065 H C K0030 131 KU024 KHUH KD024 KHDV CU009 36000 R 6105 H C K0031 127 KU013 KNUV KD013 KHDH CU011 36000 R 6145 H C K0032 127 KU015 KNUV KD015 KHDH CU013 36000 R 6185 H C K0033 127 KU017 KNUV KD017 KHDH CU015 36000 R 6225 H C K0034 127 KU014 KNUH KD014 KHDV CU017 36000 R 6265 H C K0035 127 KU016 KNUH KD016 KHDV CU019 36000 R 6305 H C K0036 127 KU018 KNUH KD018 KHDV CU021 36000 R 6345 H C K0037 129 KU013 KHUV KD013 KNDH CU023 36000 R 6385 H C K0038 129 KU015 KHUV KD015 KNDH CU002 36000 R 5965 V C K0039 129 KU017 KHUV KD017 KNDH CU004 36000 R 6005 V C K0040 129 KU014 KHUH KD014 KNDV CU006 36000 R 6045 V C K0041 129 KU016 KHUH KD016 KNDV CU008 36000 R 6085 V C K0042 129 KU018 KHUH KD018 KNDV CU010 36000 R 6125 V C C0049 119 CU001 CSUH CD001 CCDV CU012 36000 R 6165 V C C0050 119 CU003 CSUH CD003 CCDV CU014 36000 R 6205 V C C0051 119 CU005 CSUH CD005 CCDV CU016 36000 R 6245 V C C0052 119 CU007 CSUH CD007 CCDV CU018 36000 R 6285 V C C0053 119 CU009 CSUH CD009 CCDV CU020 36000 R 6325 V C C0054 119 CU011 CSUH CD011 CCDV CU022 36000 R 6365 V C TC TC OMNI CU024 36000 R 6405 V C TM1 TM1 CHDV CD001 36000 T 3720 V C TM2 TM2 CHDV CD003 36000 T 3760 V C BCN1 BCN1 KNDV CD005 36000 T 3800 V C BCN2 BCN2 KNDH CD007 36000 T 3840 V C C0001 120 CU001 CCUH CD001 CCDV CD009 36000 T 3880 V C C0002 120 CU003 CCUH CD003 CCDV CD011 36000 T 3920 V C C0003 120 CU005 CCUH CD005 CCDV

CD013 36000 T 3960 V C C0004 120 CU007 CCUH CD007 CCDV CD015 36000 T 4000 V C C0005 120 CU009 CCUH CD009 CCDV CD017 36000 T 4040 V C C0006 120 CU011 CCUH CD011 CCDV CD019 36000 T 4080 V C C0007 120 CU002 CCUV CD002 CCDH CD021 36000 T 4120 V C C0008 120 CU004 CCUV CD004 CCDH CD023 36000 T 4160 V C C0009 120 CU006 CCUV CD006 CCDH CD002 36000 T 3740 H C C0010 120 CU008 CCUV CD008 CCDH CD004 36000 T 3780 H C C0011 120 CU010 CCUV CD010 CCDH CD006 36000 T 3820 H C C0012 120 CU012 CCUV CD012 CCDH CD008 36000 T 3860 H C C0013 124 CU013 CHUH CD013 CHDV CD010 36000 T 3900 H C C0014 124 CU015 CHUH CD015 CHDV CD012 36000 T 3940 H C C0015 124 CU017 CHUH CD017 CHDV CD014 36000 T 3980 H C C0016 124 CU019 CHUH CD019 CHDV CD016 36000 T 4020 H C C0017 124 CU021 CHUH CD021 CHDV CD018 36000 T 4060 H C C0018 124 CU023 CHUH CD023 CHDV CD020 36000 T 4100 H C C0019 121 CU014 CHUV CD014 CHDH CD022 36000 T 4140 H C C0020 121 CU016 CHUV CD016 CHDH CD024 36000 T 4180 H C C0021 121 CU018 CHUV CD018 CHDH KU001 36000 R 14020 V C C0022 121 CU020 CHUV CD020 CHDH KU003 36000 R 14060 V C C0023 121 CU022 CHUV CD022 CHDH KU005 36000 R 14100 V C C0024 121 CU024 CHUV CD024 CHDH KU007 36000 R 14140 V C C0025 118 CU001 CSUH CD001 CSDV KU009 36000 R 14180 V C C0026 118 CU003 CSUH CD003 CSDV KU011 36000 R 14220 V C C0027 118 CU005 CSUH CD005 CSDV KU013 36000 R 14260 V C C0028 118 CU007 CSUH CD007 CSDV KU015 36000 R 14300 V C C0029 118 CU009 CSUH CD009 CSDV KU017 36000 R 14340 V C C0030 118 CU011 CSUH CD011 CSDV KU019 36000 R 14380 V C C0031 118 CU002 CSUV CD002 CSDH KU021 36000 R 14420 V C C0032 118 CU004 CSUV CD004 CSDH KU023 36000 R 14460 V C C0033 118 CU006 CSUV CD006 CSDH KU002 36000 R 14040 H C C0034 118 CU008 CSUV CD008 CSDH KU004 36000 R 14080 H C C0035 118 CU010 CSUV CD010 CSDH KU006 36000 R 14120 H C C0036 118 CU012 CSUV CD012 CSDH KU008 36000 R 14160 H C C0037 119 CU001 CCUH CD001 CSDV KU010 36000 R 14200 H C C0038 119 CU003 CCUH CD003 CSDV KU012 36000 R 14240 H C C0039 119 CU005 CCUH CD005 CSDV KU014 36000 R 14280 H C C0040 119 CU007 CCUH CD007 CSDV KU016 36000 R 14320 H C C0041 119 CU009 CCUH CD009 CSDV KU018 36000 R 14360 H C C0042 119 CU011 CCUH CD011 CSDV

KU020 36000 R 14400 H C C0043 119 CU002 CCUV CD002 CSDH KU022 36000 R 14440 H C C0044 119 CU004 CCUV CD004 CSDH KU024 36000 R 14480 H C C0045 119 CU006 CCUV CD006 CSDH KD001 36000 T 11720 H C C0046 119 CU008 CCUV CD008 CSDH KD003 36000 T 11760 H C C0047 119 CU010 CCUV CD010 CSDH KD005 36000 T 11800 H C C0048 119 CU012 CCUV CD012 CSDH KD007 36000 T 11840 H C C0055 119 CU002 CSUV CD002 CCDH KD009 36000 T 11880 H C C0056 119 CU004 CSUV CD004 CCDH KD011 36000 T 11920 H C C0057 119 CU006 CSUV CD006 CCDH KD013 36000 T 11960 H C C0058 119 CU008 CSUV CD008 CCDH KD015 36000 T 12000 H C C0059 119 CU010 CSUV CD010 CCDH KD017 36000 T 12040 H C C0060 119 CU012 CSUV CD012 CCDH KD019 36000 T 12080 H C K0001 125 KU001 KNUV KD001 KNDH KD021 36000 T 12120 H C K0002 125 KU003 KNUV KD003 KNDH KD023 36000 T 12160 H C K0003 125 KU005 KNUV KD005 KNDH KD002 36000 T 11740 V C K0004 125 KU007 KNUV KD007 KNDH KD004 36000 T 11780 V C K0005 125 KU009 KNUV KD009 KNDH KD006 36000 T 11820 V C K0006 125 KU011 KNUV KD011 KNDH KD008 36000 T 11860 V C K0007 125 KU013 KNUV KD013 KNDH KD010 36000 T 11900 V C K0008 125 KU015 KNUV KD015 KNDH KD012 36000 T 11940 V C K0009 125 KU017 KNUV KD017 KNDH KD014 36000 T 11980 V C K0010 125 KU002 KNUH KD002 KNDV KD016 36000 T 12020 V C K0011 125 KU004 KNUH KD004 KNDV KD018 36000 T 12060 V C K0012 125 KU006 KNUH KD006 KNDV KD020 36000 T 12100 V C K0013 125 KU008 KNUH KD008 KNDV KD022 36000 T 12140 V C K0014 125 KU010 KNUH KD010 KNDV KD024 36000 T 12180 V C K0015 125 KU012 KNUH KD012 KNDV TC 1000 R 5926 R T K0016 125 KU014 KNUH KD014 KNDV TM1 300 T 4198.875 V T K0017 125 KU016 KNUH KD016 KNDV TM2 300 T 4199.5 V T K0018 125 KU018 KNUH KD018 KNDV BCN1 25 T 11701.5 V T K0019 131 KU013 KHUV KD013 KHDH BCN2 25 T 12199 H T K0020 131 KU015 KHUV KD015 KHDH K0021 131 KU017 KHUV KD017 KHDH K0022 131 KU019 KHUV KD019 KHDH K0023 131 KU021 KHUV KD021 KHDH K0024 131 KU023 KHUV KD023 KHDH K0025 131 KU014 KHUH KD014 KHDV K0026 131 KU016 KHUH KD016 KHDV

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 146KG7W 145.9 4 128 0.5 5.9 18.1 D2 1M56G7W 1556.5 4 2048 0.75 8.2 20.4 D3 5M56G7W 5563.2 4 7320 0.75 8.2 20.4 D4 36M0G7W 36000 4 41468 0.691 6.1 18.3

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) A1 36M0F9F 36000 TV/FM 1 NTSC 12.8 1.29 12 26

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) C0001 C0012 D1 240 150 146k C-C.doc 47.5 -7.5 -1.5 11.6 17.6 -160.4 24.6 C0001 C0012 D2 22 1636 1.56M C-C.doc 47.5 2.8 8.8 21.9 27.9 -160.7 28.5 C0001 C0012 D3 6 6000 5.56M C-C.doc 47.5 12 18 27.2 33.2 -160.7 24.6 C0001 C0012 D4 1 36M C-C.doc 53.5 13.5 19.5 37.8 43.8 -158.2 24.6 C0001 C0012 A1 1 TV C-C.doc 2000 53.5 15.5 21.5 37.8 43.8 -145.6 24.6 C0013 C0024 D1 240 150 146k H-H.doc 47.5 -7.5 -1.5 9.2 15.2 -162.7 24.6 C0013 C0024 D2 22 1636 1.56M H-H.doc 47.5 2.8 8.8 19.5 25.5 -162.7 28.5 C0013 C0024 D3 6 6000 5.56M H-H.doc 47.5 12 18 24.8 30.8 -163 24.6 C0013 C0024 D4 1 36M H-H.doc 53.5 18.6 24.6 37.1 43.1 -158.8 24.6 C0013 C0024 A1 1 TV H-H.doc 2000 53.5 14.9 20.9 35 41 -148.3 24.6 C0025 C0036 D1 240 150 146k S-S.doc 47.5 -7.5 -1.5 11.1 17.1 -161.1 24.6 C0025 C0036 D2 22 1636 1.56M S-S.doc 47.5 2.8 8.8 21.4 27.4 -161.1 28.5 C0025 C0036 D3 6 6000 5.56M S-S.doc 47.5 12 18 26.7 32.7 -161.3 24.6 C0025 C0036 D4 1 36M S-S.doc 53.5 11.6 17.6 36 42 -160.1 24.6 C0025 C0036 A1 1 TV S-S.doc 2000 53.5 13.4 19.4 35.8 41.8 -147.6 24.6 C0037 C0048 D1 240 150 146k C-S.doc 47.5 -7.5 -1.5 11.1 17.1 -161.1 24.6 C0037 C0048 D2 22 1636 1.56M C-S.doc 47.5 2.8 8.8 21.4 27.4 -161.1 28.5 C0037 C0048 D3 6 6000 5.56M C-S.doc 47.5 12 18 26.7 32.7 -163.3 24.6 C0037 C0048 D4 1 36M C-S.doc 53.5 11.6 17.6 36 42 -160.1 24.6 C0037 C0048 A1 1 TV C-S.doc 2000 53.5 13.4 19.4 35.8 41.8 -147.6 24.6 C0049 C0060 D1 240 150 146k S-C.doc 47.5 -7.5 -1.5 11.6 17.6 -160.4 24.6 C0049 C0060 D2 22 1636 1.56M S-C.doc 47.5 2.8 8.8 21.9 27.9 -160.4 28.5 C0049 C0060 D3 6 6000 5.56M S-C.doc 47.5 12 18 27.2 33.2 -160.7 24.6 C0049 C0060 D4 1 36M S-C.doc 53.5 13.5 19.5 37.8 43.8 -158.2 24.6 C0049 C0060 A1 1 TV S-C.doc 2000 53.5 15.5 21.5 37.8 43.8 -145.6 24.6 K0001 K0018 D1 240 150 146k N-N.doc 43.2 -6.5 -0.5 19.2 25.2 32.8 K0001 K0018 D2 22 1636 1.56M N-N.doc 51.2 3.8 9.8 29.5 35.5 29.2 K0001 K0018 D3 6 6000 5.56M N-N.doc 53 7.8 13.8 35.3 41.3 31.1 K0001 K0018 D4 1 36M N-N.doc 54.7 15.3 21.3 44.2 50.2 21.3

K0001 K0018 A1 1 TV N-N.doc 2000 54.7 15.3 21.3 44.2 50.2 28.7 K0019 K0030 D1 240 150 146k HM-HM.d 43.2 -4.5 1.5 18 24 32.8 K0019 K0030 D2 22 1636 1.56M HM-HM. 51.2 3.8 9.8 28.3 34.3 29.2 K0019 K0030 D3 6 6000 5.56M HM-HM. 53 7.8 13.8 34.1 40.1 31.1 K0019 K0030 D4 1 36M HM-HM.do 54.7 19.1 25.1 44.9 50.9 21.3 K0019 K0030 A1 1 TV HM-HM.doc 2000 54.7 19.1 25.1 44.9 50.9 28.7 K0031 K0036 D1 240 150 146k N-HM.doc 43.2 -6.5 -0.5 18 24 32.8 K0031 K0036 D2 22 1636 1.56M N-HM.do 51.2 3.8 9.8 28.3 34.3 29.2 K0031 K0036 D3 6 6000 5.56M N-HM.do 53 7.8 13.8 34.1 40.1 31.1 K0031 K0036 D4 1 36M N-HM.doc 54.7 19.1 25.1 44.9 50.9 21.3 K0031 K0036 A1 1 TV N-HM.doc 2000 54.7 19.1 25.1 44.9 50.9 28.7 K0037 K0042 D1 240 150 146k HM-N.doc 43.2 -4.5 1.5 19.2 25.2 32.8 K0037 K0042 D2 22 1636 1.56M HM-N.do 51.2 3.8 9.8 29.5 35.5 29.2 K0037 K0042 D3 6 6000 5.56M HM-N.do 53 7.8 13.8 44.2 50.2 31.1 K0037 K0042 D4 1 36M HM-N.doc 54.7 15.3 21.3 44.2 50.2 21.3 K0037 K0042 A1 1 TV HM-N.doc 2000 54.7 15.3 21.3 44.2 50.2 28.7

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

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 2310 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3146 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5456 31.1 0.85 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1077 4.5 0.87 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 31.5 9.1 0.74 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): 9330 9330 9330 9330 Bus (Watts): (b): (g): (l): (q): 1076 820 1076 819 Total (Watts): (c): (h): (m): (r): 10406 10150 10406 10149 Solar Array (Watts): (d): (i): (n): (s): 13694 11687 12388 10664 Depth of Battery (e) (j) (o) (t) Discharge (%): 78 % 78 % 78 % 78 % 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: 2006-03-30 10:04:20
Document Modified: 2006-03-30 10:04:20
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