Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20090518-00053 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2009051800053_712920

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: ECHOSTAR-14 3/1/2010 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 1/1/2007 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 9/1/2009 146 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: 1/15/2010 2/15/2010 3504 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) 17.3 G 17.8 G R Feeder Link for Broadcasting Satellite Service in FSS 12.2 G 12.7 G T Broadcasting Satellite Service - Video 12.2 G 12.7 G T Broadcasting Satellite Service - Sound 12.2 G 12.7 G T Broadcasting Satellite Service - Data 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: 118.9 W Consistent with ITU Region 2 BSS Plan and existing Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be DISH license as this is within the 119W ±0.2° clust er N/S Station-Keeping provided (Optional): 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) CHEYENNE S Area around Cheyenne, WY GILBERT S Area around Gilbert, AZ PEORIA S Area around Peoria, IL RICHMOND S Area around Richmond, VA SAN ANTONIO S Area around San Antonio, TX SPOKANE S Area around Spokane, WA CONUS S CONUS ALASKA S Alaska HAWAII S Hawaii PUERTO RICO S Puerto Rico CUBA S Cuba CONUS+ S CONUS, Alaska, Hawaii, Puerto Rico & Cuba GLOBAL 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) R1 R 49.6 46.6 0.12 0.12 30 N CHEYENN 4748 12.8 -106 21 0.5 R2 R 48.4 45.4 0.12 0.12 30 N GILBERT 4836 11.6 -106 21 0.5 R3 R 48.1 45.1 0.12 0.12 30 N RICHMON 2911 13.4 -106 21 0.5 R4 R 47.2 44.2 0.12 0.12 30 N PEORIA 2964 12.4 -106 21 0.5 R5 R 44.4 41.4 0.12 0.12 30 N SPOKANE 2117 11.2 -106 21 0.5 R6 R 46.4 43.4 0.12 0.12 30 N SAN ANT 3181 11.4 -106 21 0.5 TC1L T 36.2 21.2 0.12 0.12 30 N CONUS+ 2.2 269.2 60.5 TC1R T 36.4 21.4 0.12 0.12 30 N CONUS+ 2.2 269.2 60.7 TC2L T 36.1 21.1 0.12 0.12 30 N CONUS+ 2.3 263 60.3 TC2R T 36.1 21.1 0.12 0.12 30 N CONUS+ 2.4 257 60.2 A01 T 44.8 41.7 0.05 0.12 30 N CONUS 2 6.8 53.2 A02 T 44.5 40.9 0.05 0.12 30 N CONUS 2 8.2 53.6 A03 T 43.4 38.6 0.05 0.12 30 N CONUS 2 13.8 54.9 A04 T 45.1 39.4 0.05 0.12 30 N CONUS 2 11.5 55.8 A05 T 42.9 39.9 0.05 0.12 30 N CONUS 2 10.2 52.9 A06 T 43.5 38.7 0.05 0.12 30 N CONUS 2 13.4 54.8 A07 T 42.6 35.4 0.05 0.12 30 N CONUS 2 28.8 57.2 A08 T 45.9 40.1 0.05 0.12 30 N CONUS 2 9.8 55.8 A09 T 44.7 37.4 0.05 0.12 30 N CONUS 2 18.3 57.3 A10 T 47.6 39.8 0.05 0.12 30 N CONUS 2 10.5 57.8 A11 T 46.1 36.8 0.05 0.12 30 N CONUS 2 20.8 59.3 A12 T 46.1 38.5 0.05 0.12 30 N CONUS 2 14.1 57.6 A13 T 43.1 34.9 0.05 0.12 30 N CONUS 2 32.4 58.2 A14 T 45.7 35.8 0.05 0.12 30 N CONUS 2 26 59.9 A15 T 44.6 37.1 0.05 0.12 30 N CONUS 2 19.4 57.4 A16 T 46.2 37.6 0.05 0.12 30 N CONUS 2 17.2 58.6 A17 T 46.7 36.8 0.05 0.12 20 N CONUS 2 21 59.9 A18 T 46.6 37 0.05 0.12 30 N CONUS 2 19.9 59.6 A19 T 45 37.2 0.05 0.12 30 N CONUS 2 19.1 57.8

A20 T 47.1 38.6 0.05 0.12 30 N CONUS 2 13.8 58.6 A21 T 42.6 38.3 0.05 0.12 30 N CONUS 2 14.8 54.3 A22 T 43.9 39.3 0.05 0.12 30 N CONUS 2 11.8 54.6 A23 T 47.5 41.6 0.05 0.12 30 N CONUS 2 7 56 A24 T 43.2 36.7 0.05 0.12 30 N ALASKA 2 8.6 52.6 A25 T 43.2 36.9 0.05 0.12 30 N ALASKA 2 8.1 52.3 A26 T 42.6 36.7 0.05 0.12 30 N CUBA 2 8.5 51.9 A27 T 41.7 35.7 0.05 0.12 30 N HAWAII 2 10.7 52 A28 T 41.7 35.7 0.05 0.12 30 N HAWAII 2 10.7 52 B01 T 45.1 38.7 0.05 0.12 30 N CONUS 2 13.4 56.4 B02 T 44.6 38.1 0.05 0.12 30 N CONUS 2 15.5 56.5 B03 T 44.6 36.8 0.05 0.12 30 N CONUS 2 20.8 57.8 B04 T 46.1 42.5 0.05 0.12 30 N CONUS 2 5.6 53.6 B05 T 47.7 36.6 0.05 0.12 30 N CONUS 2 21.8 61.1 B06 T 43.8 38.8 0.05 0.12 30 N CONUS 2 13.1 55 B07 T 44.1 36.8 0.05 0.12 30 N CONUS 2 20.8 57.3 B08 T 42.6 39 0.05 0.12 30 N CONUS 2 12.5 53.6 B09 T 44.6 35.5 0.05 0.12 30 N CONUS 2 28.2 59.1 B10 T 44.9 35.8 0.05 0.12 30 N CONUS 2 26.4 59.2 B11 T 44.5 36 0.05 0.12 30 N CONUS 2 25.2 58.5 B12 T 44.9 37.9 0.05 0.12 30 N CONUS 2 16.2 57 B13 T 44.1 35.2 0.05 0.12 30 N CONUS 2 30.5 59 B14 T 44.8 35 0.05 0.12 30 N CONUS 2 31.6 59.8 B15 T 46.2 35.5 0.05 0.12 30 N CONUS 2 28.2 60.7 B16 T 46 37.2 0.05 0.12 30 N CONUS 2 19.2 58.9 B17 T 48.2 40.1 0.05 0.12 30 N CONUS 2 9.7 58 B18 T 47 36.4 0.05 0.12 30 N CONUS 2 22.7 60.5 B19 T 47.8 37.6 0.05 0.12 30 N CONUS 2 17.5 60.2 B20 T 45.6 36.3 0.05 0.12 30 N CONUS 2 23.6 59.4 B21 T 47.2 39.7 0.05 0.12 30 N CONUS 2 10.7 57.5 B22 T 44.9 39.7 0.05 0.12 30 N PUERTO 2 4.2 51.2 B23 T 46.6 42.2 0.05 0.12 30 N PUERTO 2 2.4 50.4 OMN R 9 -1 30 N GLOBAL 4365 -27.4 -83 OMN T 5 -4 30 N GLOBAL 3.6 15.1 16.8 GBL R 25.25 24.25 0.12 0.12 30 N GLOBAL 13804 -16.2 -93

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) R01 24000 R 17324.00 R C 001 127 R01 R1 T01 TC1R R03 24000 R 17353.16 R C 002 127 R02 R1 T02 TC2L R05 24000 R 17382.32 R C 003 127 R03 R1 T03 TC2R R07 24000 R 17411.48 R C 004 127 R04 R1 T04 TC1L R09 24000 R 17440.64 R C 005 127 R05 R1 T05 TC1R R11 24000 R 17469.80 R C 006 127 R06 R1 T06 TC2L R13 24000 R 17498.96 R C 007 127 R07 R1 T07 TC2R R15 24000 R 17528.12 R C 008 127 R08 R1 T08 TC1L R17 24000 R 17557.28 R C 009 127 R09 R1 T09 TC1R R19 24000 R 17586.44 R C 010 127 R10 R1 T10 TC2L R21 24000 R 17615.60 R C 011 127 R11 R1 T11 TC2R R23 24000 R 17644.76 R C 012 127 R12 R1 T12 TC1L R25 24000 R 17673.92 R C 013 127 R13 R1 T13 TC1R R27 24000 R 17703.08 R C 014 127 R14 R1 T14 TC2L R29 24000 R 17732.24 R C 015 127 R15 R1 T15 TC2R R31 24000 R 17761.40 R C 016 127 R16 R1 T16 TC1L R02 24000 R 17338.58 L C 017 127 R17 R1 T17 TC1R R04 24000 R 17367.74 L C 018 127 R18 R1 T18 TC2L R06 24000 R 17396.90 L C 019 127 R19 R1 T19 TC2R R08 24000 R 17426.06 L C 020 127 R20 R1 T20 TC1L R10 24000 R 17455.22 L C 021 127 R21 R1 T21 TC1R R12 24000 R 17484.38 L C 022 127 R22 R1 T22 TC2L R14 24000 R 17513.54 L C 023 127 R23 R1 T23 TC2R R16 24000 R 17542.70 L C 024 127 R24 R1 T24 TC1L R18 24000 R 17571.86 L C 025 127 R25 R1 T25 TC1R R20 24000 R 17601.02 L C 026 127 R26 R1 T26 TC2L R22 24000 R 17630.18 L C 027 127 R27 R1 T27 TC2R R24 24000 R 17659.34 L C 028 127 R28 R1 T28 TC1L R26 24000 R 17688.50 L C 029 127 R29 R1 T29 TC1R R28 24000 R 17717.66 L C 030 127 R30 R1 T30 TC2L

R30 24000 R 17746.82 L C 031 127 R31 R1 T31 TC2R R32 24000 R 17775.98 L C 032 127 R32 R1 T32 TC1L T01 24000 T 12224.00 R C 033 128 R01 R2 T01 TC1R T03 24000 T 12253.16 R C 034 128 R02 R2 T02 TC2L T05 24000 T 12282.32 R C 035 128 R03 R2 T03 TC2R T07 24000 T 12311.48 R C 036 128 R04 R2 T04 TC1L T09 24000 T 12340.64 R C 037 128 R05 R2 T05 TC1R T11 24000 T 12369.80 R C 038 128 R06 R2 T06 TC2L T13 24000 T 12398.96 R C 039 128 R07 R2 T07 TC2R T15 24000 T 12428.12 R C 040 128 R08 R2 T08 TC1L T17 24000 T 12457.28 R C 041 128 R09 R2 T09 TC1R T19 24000 T 12486.44 R C 042 128 R10 R2 T10 TC2L T21 24000 T 12515.60 R C 043 128 R11 R2 T11 TC2R T23 24000 T 12544.76 R C 044 128 R12 R2 T12 TC1L T25 24000 T 12573.92 R C 045 128 R13 R2 T13 TC1R T27 24000 T 12603.08 R C 046 128 R14 R2 T14 TC2L T29 24000 T 12632.24 R C 047 128 R15 R2 T15 TC2R T31 24000 T 12661.40 R C 048 128 R16 R2 T16 TC1L T02 24000 T 12238.58 L C 049 128 R17 R2 T17 TC1R T04 24000 T 12267.74 L C 050 128 R18 R2 T18 TC2L T06 24000 T 12296.90 L C 051 128 R19 R2 T19 TC2R T08 24000 T 12326.06 L C 052 128 R20 R2 T20 TC1L T10 24000 T 12355.22 L C 053 128 R21 R2 T21 TC1R T12 24000 T 12384.38 L C 054 128 R22 R2 T22 TC2L T14 24000 T 12413.54 L C 055 128 R23 R2 T23 TC2R T16 24000 T 12442.70 L C 056 128 R24 R2 T24 TC1L T18 24000 T 12471.86 L C 057 128 R25 R2 T25 TC1R T20 24000 T 12501.02 L C 058 128 R26 R2 T26 TC2L T22 24000 T 12530.18 L C 059 128 R27 R2 T27 TC2R T24 24000 T 12559.34 L C 060 128 R28 R2 T28 TC1L T26 24000 T 12588.50 L C 061 128 R29 R2 T29 TC1R T28 24000 T 12617.66 L C 062 128 R30 R2 T30 TC2L T30 24000 T 12646.82 L C 063 128 R31 R2 T31 TC2R T32 24000 T 12675.98 L C 064 128 R32 R2 T32 TC1L CMD1 1000 R 17794 R T 065 115 R19 R5 T05 A01 CMD2 1000 R 17797 R T 066 115 R12 R5 T02 A02 TLM1 1000 T 12692 R T 067 115 R14 R5 T04 A02 TLM2 1000 T 12698.5 R T 068 115 R16 R5 T06 A02 RFB 30 R 17799.75 R T 069 115 R02 R5 T02 A03

070 115 R04 R5 T04 A03 071 115 R06 R5 T06 A03 072 115 R05 R5 T05 A04 073 115 R07 R5 T07 A04 074 115 R09 R5 T09 A04 075 115 R11 R5 T11 A04 076 115 R04 R6 T04 A05 077 115 R06 R6 T06 A05 078 115 R08 R2 T08 A06 079 115 R21 R5 T07 A01 080 115 R20 R6 T13 A07 081 115 R15 R4 T01 A07 082 115 R21 R4 T07 A07 083 115 R02 R2 T02 A08 084 115 R14 R6 T04 A09 085 115 R12 R6 T02 A10 086 115 R01 R4 T01 A11 087 115 R07 R4 T07 A11 088 115 R09 R4 T09 A11 089 115 R13 R4 T13 A11 090 115 R02 R4 T02 A12 091 115 R08 R4 T08 A12 092 115 R01 R6 T01 A13 093 115 R07 R6 T07 A13 094 115 R09 R6 T09 A13 095 115 R13 R6 T13 A13 096 115 R02 R6 T02 A14 097 115 R08 R6 T08 A14 098 115 R10 R6 T10 A14 099 115 R01 R3 T01 A15 100 115 R07 R3 T07 A15 101 115 R02 R3 T02 A16 102 115 R18 R6 T11 A17 103 115 R21 R6 T07 A17 104 115 R15 R3 T01 A17 105 115 R12 R3 T02 A18 106 115 R06 R2 T02 A19 107 115 R15 R6 T01 A20 108 115 R19 R6 T05 A20

109 115 R13 R1 T13 A21 110 115 R15 R5 T01 A21 111 115 R11 R2 T05 A22 112 115 R21 R2 T07 A23 113 115 R01 R2 T01 A24 114 115 R03 R2 T03 A24 115 115 R05 R2 T05 A24 116 115 R04 R2 T04 A25 117 115 R10 R2 T10 A25 118 115 R07 R2 T01 A26 119 115 R19 R3 T05 A26 120 115 R15 R2 T01 A27 121 115 R17 R2 T03 A27 122 115 R19 R2 T05 A27 123 115 R12 R2 T02 A28 124 115 R14 R2 T04 A28 125 115 R08 R5 T08 B01 126 115 R10 R5 T10 B01 127 115 R17 R5 T03 B02 128 115 R01 R5 T01 B03 129 115 R03 R5 T03 B03 130 115 R13 R5 T13 B03 131 115 R02 R1 T02 B04 132 115 R08 R1 T08 B04 133 115 R16 R6 T09 B05 134 115 R20 R5 T10 B06 135 115 R03 R1 T03 B07 136 115 R09 R1 T09 B07 137 115 R11 R1 T11 B07 138 115 R12 R4 T02 B08 139 115 R06 R1 T06 B09 140 115 R10 R1 T10 B09 141 115 R18 R4 T08 B09 142 115 R03 R6 T03 B10 143 115 R05 R6 T05 B10 144 115 R11 R6 T11 B10 145 115 R16 R2 T06 B11 146 115 R18 R2 T08 B11 147 115 R04 R4 T04 B12

148 115 R06 R4 T06 B12 149 115 R10 R4 T10 B12 150 115 R03 R4 T03 B13 151 115 R05 R4 T05 B13 152 115 R11 R4 T11 B13 153 115 R14 R4 T04 B14 154 115 R16 R4 T06 B14 155 115 R20 R4 T10 B14 156 115 R17 R4 T03 B15 157 115 R19 R4 T05 B15 158 115 R03 R3 T03 B16 159 115 R05 R3 T05 B16 160 115 R09 R3 T09 B16 161 115 R11 R3 T11 B16 162 115 R13 R3 T13 B16 163 115 R04 R3 T04 B17 164 115 R06 R3 T06 B17 165 115 R08 R3 T08 B17 166 115 R10 R3 T10 B17 167 115 R14 R3 T04 B18 168 115 R16 R3 T06 B18 169 115 R20 R3 T10 B18 170 115 R09 R2 T09 B19 171 115 R13 R2 T13 B19 172 115 R18 R3 T04 B20 173 115 R17 R3 T03 B21 174 115 R21 R3 T07 B21 175 115 R01 R1 T01 B22 176 115 R05 R1 T05 B22 177 115 R07 R1 T07 B22 178 115 R04 R1 T04 B23 CMDA CMD1 OMNR CMDB CMD2 OMNR CMDC CMD1 GBLR CMDD CMD2 GBLR TLMA TLM1 OMNT TLMB TLM2 OMNT TLMC TLM1 TC1R TLMD TLM2 TC1R

179 115 R05 R5 T05 A01 180 115 R19 R5 T05 A04 181 115 R09 R6 T01 A07 182 115 R13 R6 T05 A07 183 115 R02 R1 T02 A08 184 115 R02 R6 T02 A10 185 115 R05 R4 T05 A11 186 115 R12 R6 T02 A14 187 115 R08 R3 T01 A17 188 115 R10 R3 T03 A17 189 115 R15 R4 T01 A23 190 115 R02 R2 T02 A25 191 115 R15 R5 T01 B02 192 115 R17 R6 T03 B07 193 115 R08 R2 T04 B09 194 115 R14 R6 T04 B11 195 115 R17 R4 T03 B13 196 115 R16 R3 T02 B20 197 115 R03 R1 T03 B22 RFB1 RFB R1 RFB2 RFB R2

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) QPSK1 24M0G7W 24000 4 27647 0.6912 0 5.7 28 QPSK2 24M0G7W 24000 4 30719 0.768 0 6.6 28 8PSK1 25M8G7W 25800 8 41200 0.6389 0 7.5 28

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) CMD1 1M00F2D 1000 1 10 22.2 TLM1 1M00G2D 1000 1 9 21.2 RFB 30K0N0N 30 1 14 26.2

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) 001 178 QPSK1 1 E-14 Link Budg 001 178 QPSK2 1 E-14 Link Budg 001 178 8PSK1 1 E-14 Link Budg CMDA CMDB CMD1 1 E-14 Link Budg 64 16.3 39.3 -37.4 CMDC CMDD CMD1 1 E-14 Link Budg 64 5.8 15.8 -17.2 TLMA TLMB TLM1 1 E-14 Link Budg 7.8 16.8 42 TLMC TLMD TLM1 1 E-14 Link Budg 17.3 27 37 RFB1 RFB2 RFB 1 E-14 Link Budg 64 -5.2 1.8

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: 530 Echostar Drive S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Cheyenne Laramie WY 82007 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 307-633-5460 Remote Control (TT C) Location(s): S14a: Street Address: 801 North Dish Drive S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Gilbert Maricopa AZ 85233 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 480-558-2778

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 3223 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3085 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6308 32.4 0.721 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 3080 12 0.832 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 90 8.2 0.6 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): 14410 14410 14410 14410 Bus (Watts): (b): (g): (l): (q): 3429 1636 Total (Watts): (c): (h): (m): (r): 17839 16046 Solar Array (Watts): (d): (i): (n): (s): 21696 19349 19393 17449 Depth of Battery (e) (j) (o) (t) Discharge (%): 76.5 % 0 % 76.5 % 0 % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: YES NO X 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: 2009-05-22 11:11:45
Document Modified: 2009-05-22 11:11:45
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