Attachment Sched S Tech Report

This document pretains to SAT-LOA-20100310-00043 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2010031000043_805426

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-15 7/17/2010 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 4/14/2008 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 5/13/2010 32 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: 7/1/2010 10/1/2010 768 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) 17300 M 17800 M R Feeder Link for Broadcasting Satellite Service in FSS 12200 M 12700 M T Broadcasting Satellite Service - Video 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: 61.55 W Consistent with Region 2 USA Plan and existing Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be EchoStar license. N/S Station-Keeping provided (Optional): d. Toward West: Degrees E/W 0.05 Degrees Tolerance: g. Westernmost: W e. Toward East: 0.05 Degrees 0.05 Degrees h. Easternmost: W i. Reason for service are selection (Optional): Cluster range of Region 2 BSS Plan for the 61.5W nominal orbital slot is from 61.7W to 61.3W.

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, Puerto Rico CHEYENNE S Area around Cheyenne, WY GILBERT S Area around Gilbert, AZ 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) OMN R 9 -4 1 1 30 N GLOBAL 5000 -41 -83 OMN T 9 -4 1 1 30 N GLOBAL 9.3 4.1 15.2 TCO R 44.9 41.9 0.12 0.2 30 N CHEYENN 32000 -10 -93 NA T 0 0 0 0 30 CONUS+ 1 1 0 TCO R 44.7 41.9 0.12 0.2 30 N GILBERT 32000 -10 -93 RR1 R 44.9 41.9 0.12 0.2 30 N CHEYENN 1905 7.6 -100.4 21 1 RL1 R 44.9 41.9 0.12 0.2 30 N CHEYENN 1905 7.6 -100.4 21 1 RR2 R 44.7 41.7 0.12 0.2 30 N GILBERT 1919 7.4 -99.5 21 1 TEL T 34.3 24.3 0.12 0.2 30 N CONUS+ 2.8 236 58.1 TER T 34.3 24.3 0.12 0.2 30 N CONUS+ 2.8 236 58.1 TMO T 34.3 28.3 0.12 0.2 30 N CONUS+ 4.9 0.13 18 TMO T 34.3 28.3 0.12 0.2 30 N CONUS+ 4.9 0.13 18 RL2 R 44.7 41.7 0.12 0.2 30 N GILBERT 1919 7.4 -99.5 21 1 TWL T 34.3 24.3 0.12 0.2 30 N CONUS+ 2.8 236 58.1 TWR T 34.3 24.3 0.12 0.2 30 N CONUS+ 2.8 236 58.1

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) TCO R C -61.55 TCOS1.gxt TCO R C -61.55 TCOS2.gxt RL1 R C -61.55 RL1.gxt RR2 R C -61.55 RR2.gxt RL2 R C -61.55 RL2.gxt TEL T C -61.55 TEL.gxt TER T C -61.55 TER.gxt TWL T C -61.55 TWL.gxt TWR T C -61.55 TWR.gxt RR1 R C -61.55 RR1.gxt TMO T C -61.55 TMOS1.gxt TMO T C -61.55 TMOS2.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) R01 24000 R 17324 R C H01 125.6 R01 RR1 T01 TER R03 24000 R 17353.16 R C H03 125.6 R03 RR1 T03 TWR R05 24000 R 17382.32 R C H05 125.6 R05 RR1 T05 TER R07 24000 R 17411.48 R C H07 125.6 R07 RR1 T07 TWR R09 24000 R 17440.64 R C H09 125.6 R09 RR1 T09 TER R11 24000 R 17469.8 R C H11 125.6 R11 RR1 T11 TWR R13 24000 R 17498.96 R C H13 125.6 R13 RR1 T13 TER R15 24000 R 17528.12 R C H15 125.6 R15 RR1 T15 TWR R17 24000 R 17557.28 R C H17 125.6 R17 RR1 T17 TER R19 24000 R 17586.44 R C H19 125.6 R19 RR1 T19 TWR R21 24000 R 17615.6 R C H21 125.6 R21 RR1 T21 TER R23 24000 R 17644.76 R C H23 125.6 R23 RR1 T23 TWR R25 24000 R 17673.92 R C H25 125.6 R25 RR1 T25 TER R27 24000 R 17703.08 R C H27 125.6 R27 RR1 T27 TWR R29 24000 R 17732.24 R C H29 125.6 R29 RR1 T29 TER R31 24000 R 17761.4 R C H31 125.6 R31 RR1 T31 TWR R02 24000 R 17338.58 L C H02 125.6 R02 RL1 T02 TWL R04 24000 R 17367.74 L C H04 125.6 R04 RL1 T04 TEL R06 24000 R 17396.9 L C H06 125.6 R06 RL1 T06 TWL R08 24000 R 17426.06 L C H08 125.6 R08 RL1 T08 TEL R10 24000 R 17455.22 L C H10 125.6 R10 RL1 T10 TWL R12 24000 R 17484.38 L C H12 125.6 R12 RL1 T12 TEL R14 24000 R 17513.54 L C H14 125.6 R14 RL1 T14 TWL R16 24000 R 17542.7 L C H16 125.6 R16 RL1 T16 TEL R18 24000 R 17571.86 L C H18 125.6 R18 RL1 T18 TWL R20 24000 R 17601.02 L C H20 125.6 R20 RL1 T20 TEL R22 24000 R 17630.18 L C H22 125.6 R22 RL1 T22 TWL R24 24000 R 17659.34 L C H24 125.6 R24 RL1 T24 TEL R26 24000 R 17688.5 L C H26 125.6 R26 RL1 T26 TWL R28 24000 R 17717.66 L C H28 125.6 R28 RL1 T28 TEL

R30 24000 R 17746.82 L C H30 125.6 R30 RL1 T30 TWL R32 24000 R 17775.98 L C H32 125.6 R32 RL1 T32 TEL T01 24000 T 12224 R C TLMF TLM4 TMOS1 T03 24000 T 12253.16 R C TLMG TLM1 TMOS2 T05 24000 T 12282.32 R C TLMH TLM2 TMOS2 T07 24000 T 12311.48 R C CMDA CMD1 OMNR T09 24000 T 12340.64 R C CMDB CMD2 OMNR T11 24000 T 12369.8 R C CMDC CMD1 TCOS1 T13 24000 T 12398.96 R C CMDD CMD1 TCOS2 T15 24000 T 12428.12 R C CMDE CMD2 TCOS1 T17 24000 T 12457.28 R C CMDF CMD2 TCOS2 T19 24000 T 12486.44 R C TLMA TLM1 OMNT T21 24000 T 12515.6 R C TLMB TLM2 OMNT T23 24000 T 12544.76 R C TLMC TLM3 OMNT T25 24000 T 12573.92 R C TLMD TLM4 OMNT T27 24000 T 12603.08 R C TLME TLM3 TMOS1 T29 24000 T 12632.24 R C H33 124.9 R01 RR2 T01 TER T31 24000 T 12661.4 R C H35 124.9 R03 RR2 T03 TWR T02 24000 T 12238.58 L C H37 124.9 R05 RR2 T05 TER T04 24000 T 12267.74 L C H39 124.9 R07 RR2 T07 TWR T06 24000 T 12296.90 L C H41 124.9 R09 RR2 T09 TER T08 24000 T 12326.06 L C H43 124.9 R11 RR2 T11 TWR T10 24000 T 12355.22 L C H45 124.9 R13 RR2 T13 TER T12 24000 T 12384.38 L C H47 124.9 R15 RR2 T15 TWR T14 24000 T 12413.54 L C H49 124.9 R17 RR2 T17 TER T16 24000 T 12442.7 L C H51 124.9 R19 RR2 T19 TWR T18 24000 T 12471.86 L C H53 124.9 R21 RR2 T21 TER T20 24000 T 12501.02 L C H55 124.9 R23 RR2 T23 TWR T22 24000 T 12530.18 L C H57 124.9 R25 RR2 T25 TER T24 24000 T 12559.34 L C H59 124.9 R27 RR2 T27 TWR T26 24000 T 12588.5 L C H61 124.9 R29 RR2 T29 TER T28 24000 T 12617.66 L C H63 124.9 R31 RR2 T31 TWR T30 24000 T 12646.82 L C H34 124.9 R02 RL2 T02 TWL T32 24000 T 12675.98 L C H36 124.9 R04 RL2 T04 TEL CMD1 1000 R 17791.5 R T H38 124.9 R06 RL2 T06 TWL CMD2 1000 R 17793.5 R T H40 124.9 R08 RL2 T08 TEL TLM1 1000 T 12692 R T H42 124.9 R10 RL2 T10 TWL TLM2 1000 T 12693 R T H44 124.9 R12 RL2 T12 TEL TLM3 1000 T 12694.5 R T H46 124.9 R14 RL2 T14 TWL

TLM4 1000 T 12698.5 R T H48 124.9 R16 RL2 T16 TEL H50 124.9 R18 RL2 T18 TWL H52 124.9 R20 RL2 T20 TEL H54 124.9 R22 RL2 T22 TWL H56 124.9 R24 RL2 T24 TEL H58 124.9 R26 RL2 T26 TWL H60 124.9 R28 RL2 T28 TEL H62 124.9 R30 RL2 T30 TWL H64 124.9 R32 RL2 T32 TEL

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 32255 0.8064 0 7.5 28 8PSK1 25M8G7W 25800 8 41209 0.6406 0 7.5 28 8PSK2 25M8G7W 25800 8 46360 0.7207 0 8.3 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) CMD 1M00F2D 1000 1 10 22.2 TLM 1M00G2D 1000 1 9 21.2

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) H01 H64 QPSK1 1 E15_LB_QPSK 65.7 4.1 16.1 46 58.1 13.2 H01 H64 QPSK2 1 E15_LB_QPSK 65.7 4.1 16.1 46 58.1 13.2 H01 H64 8PSK1 1 E15_LB_8PSK 65.7 4.1 16.1 46 58.1 13.2 CMDA CMDB CMD 1 E15_TCTO.xls 63.9 16.4 36.4 -41 CMDC CMDF CMD 1 E15_TCOS.xls 63.9 2.9 8.9 -10 TLMA TLMD TLM 1 E15_TMTO.xls 4.6 15.2 48 TLME TLMH TLM 1 E15_TMOS.xls 14 18 48 H01 H64 8PSK2 1 E15_LB_8PSK 65.7 4.1 16.1 46 58.1 13.2

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 2479 (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: 5619 6.9 0.8377 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1030 8 0.8635 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 92 32.5 0.7234 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): 14102 14102 14102 14102 Bus (Watts): (b): (g): (l): (q): 3461 1705 3461 1705 Total (Watts): (c): (h): (m): (r): 17563 15807 17563 15807 Solar Array (Watts): (d): (i): (n): (s): 19493 17522 18478 16610 Depth of Battery (e) (j) (o) (t) Discharge (%): 76.5 % 76.5 % 76.5 % 76.5 % 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: 2010-03-11 12:17:20
Document Modified: 2010-03-11 12:17:20
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