Attachment Schedule S Tech Data

This document pretains to SAT-AMD-20080114-00022 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2008011400022_616683

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 EX-4 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 12 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 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: 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) 24.75 G 25.25 G R Feeder Link for Broadcasting Satellite Service in FSS 17.3 G 17.8 G 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: 76 W See section A.2 of Attachment A ("Technical Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Information to Supplement Schedule S"). 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) SA1 S Arizona + Wyoming SA2 S CONUS + Puerto Rico SA3 S ITU Region 2, excluding territories of the United States SA4 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) RXR R 40.1 38.1 0.12 0.1 25 N SA1 600 12.3 -98.1 20 0.5 RXL R 40.1 38.1 0.12 0.1 25 N SA1 600 12.3 -98.1 20 0.5 TX1R T 37.8 29.8 0.12 0.1 25 N SA2 2.3 178 60.3 TX1L T 37.8 29.8 0.12 0.1 25 N SA2 2.3 178 60.3 TX2R T 36.4 30.4 0.12 0.1 25 N SA3 2.3 178 58.9 TX2L T 36.4 30.4 0.12 0.1 25 N SA3 2.3 178 58.9 GBL R 19.7 16.7 0.12 0.1 30 N 90 SA4 2400 -14.1 GBL T 19.7 16.7 0.12 0.1 30 N 90 SA4 5.7 5.4 27 OMN R 4 0 0.12 0.1 30 N 0 SA4 3162 -31 OMN T 4 0 0.12 0.1 30 N 90 SA4 3 8 13

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) RXR R C -76 RXR.gxt RXL R C -76 RXL.gxt TX1R T C -76 TX1R.gxt -129.4 -127 -124.2 -122.8 -121.9 TX1L T C -76 TX1L.gxt -129.4 -127 -124.2 -122.8 -121.9 TX2R T C -76 TX2R.gxt -117.6 -117.5 -117.3 -117.2 -117.1 TX2L T C -76 TX2L.gxt -117.6 -117.5 -117.3 -117.2 -117.1 GBL R C -76 GBLU.gxt GBL T C -76 GBLD.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) U0001 24000 R 24772 R C T0001 130 U0001 RXR D0001 TX1R U0003 24000 R 24801.16 R C T0003 130 U0003 RXR D0003 TX1R U0005 24000 R 24830.32 R C T0005 130 U0005 RXR D0005 TX1R U0007 24000 R 24859.48 R C T0007 130 U0007 RXR D0007 TX1R U0009 24000 R 24888.64 R C T0009 130 U0009 RXR D0009 TX1R U0011 24000 R 24917.8 R C T0011 130 U0011 RXR D0011 TX1R U0013 24000 R 24946.96 R C T0013 130 U0013 RXR D0013 TX1R U0015 24000 R 24976.12 R C T0015 130 U0015 RXR D0015 TX1R U0017 24000 R 25005.28 R C T0017 130 U0017 RXR D0017 TX1R U0019 24000 R 25034.44 R C T0019 130 U0019 RXR D0019 TX1R U0021 24000 R 25063.6 R C T0021 130 U0021 RXR D0021 TX1R U0023 24000 R 25092.76 R C T0023 130 U0023 RXR D0023 TX1R U0025 24000 R 25121.92 R C T0025 130 U0025 RXR D0025 TX1R U0027 24000 R 25151.08 R C T0002 130 U0002 RXL D0002 TX1L U0029 24000 R 25180.24 R C T0004 130 U0004 RXL D0004 TX1L U0031 24000 R 25209.4 R C T0006 130 U0006 RXL D0006 TX1L U0002 24000 R 24786.58 L C T0008 130 U0008 RXL D0008 TX1L U0004 24000 R 24815.74 L C T0010 130 U0010 RXL D0010 TX1L U0006 24000 R 24844.9 L C T0012 130 U0012 RXL D0012 TX1L U0008 24000 R 24874.06 L C T0014 130 U0014 RXL D0014 TX1L U0010 24000 R 24903.22 L C T0016 130 U0016 RXL D0016 TX1L U0012 24000 R 24932.38 L C T0018 130 U0018 RXL D0018 TX1L U0014 24000 R 24961.54 L C T0020 130 U0020 RXL D0020 TX1L U0016 24000 R 24990.7 L C T0022 130 U0022 RXL D0022 TX1L U0018 24000 R 25019.86 L C T0024 130 U0024 RXL D0024 TX1L U0020 24000 R 25049.02 L C T0026 130 U0026 RXL D0026 TX1L U0022 24000 R 25078.18 L C T0027 130 U0001 RXR D0001 TX2R U0024 24000 R 25107.34 L C T0029 130 U0003 RXR D0003 TX2R U0026 24000 R 25136.5 L C T0031 130 U0005 RXR D0005 TX2R U0028 24000 R 25165.66 L C T0033 130 U0007 RXR D0007 TX2R

U0030 24000 R 25194.82 L C T0035 130 U0009 RXR D0009 TX2R U0032 24000 R 25223.98 L C T0037 130 U0011 RXR D0011 TX2R D0001 24000 T 17322 R C T0039 130 U0013 RXR D0013 TX2R D0003 24000 T 17351.16 R C T0041 130 U0015 RXR D0015 TX2R D0005 24000 T 17380.32 R C T0043 130 U0017 RXR D0017 TX2R D0007 24000 T 17409.48 R C T0045 130 U0019 RXR D0019 TX2R D0009 24000 T 17438.64 R C T0047 130 U0021 RXR D0021 TX2R D0011 24000 T 17467.8 R C T0049 130 U0023 RXR D0023 TX2R D0013 24000 T 17496.96 R C T0051 130 U0025 RXR D0025 TX2R D0015 24000 T 17526.12 R C T0053 130 U0027 RXR D0027 TX2R D0017 24000 T 17555.28 R C T0055 130 U0029 RXR D0029 TX2R D0019 24000 T 17584.44 R C T0057 130 U0031 RXR D0031 TX2R D0021 24000 T 17613.6 R C T0028 130 U0002 RXL D0002 TX2L D0023 24000 T 17642.76 R C T0030 130 U0004 RXL D0004 TX2L D0025 24000 T 17671.92 R C T0032 130 U0006 RXL D0006 TX2L D0027 24000 T 17701.08 R C T0034 130 U0008 RXL D0008 TX2L D0029 24000 T 17730.24 R C T0036 130 U0010 RXL D0010 TX2L D0031 24000 T 17759.4 R C T0038 130 U0012 RXL D0012 TX2L D0002 24000 T 17336.58 L C T0040 130 U0014 RXL D0014 TX2L D0004 24000 T 17365.74 L C T0042 130 U0016 RXL D0016 TX2L D0006 24000 T 17394.9 L C T0044 130 U0018 RXL D0018 TX2L D0008 24000 T 17424.06 L C T0046 130 U0020 RXL D0020 TX2L D0010 24000 T 17453.22 L C T0048 130 U0022 RXL D0022 TX2L D0012 24000 T 17482.38 L C T0050 130 U0024 RXL D0024 TX2L D0014 24000 T 17511.54 L C T0052 130 U0026 RXL D0026 TX2L D0016 24000 T 17540.7 L C T0054 130 U0028 RXL D0028 TX2L D0018 24000 T 17569.86 L C T0056 130 U0030 RXL D0030 TX2L D0020 24000 T 17599.02 L C T0058 130 U0032 RXL D0032 TX2L D0022 24000 T 17628.18 L C TC1 CMD1 GBLU D0024 24000 T 17657.34 L C TC2 CMD2 GBLU D0026 24000 T 17686.5 L C TC3 CMD3 OMNUH D0028 24000 T 17715.66 L C TC4 CMD4 OMNUH D0030 24000 T 17744.82 L C TM1 TLM1 GBLD D0032 24000 T 17773.98 L C TM2 TLM2 GBLD CMD1 1000 R 24752 V T TM3 TLM1 OMNDV CMD2 1000 R 25248 V T TM4 TLM2 OMNDV CMD3 1000 R 17309 H T CMD4 1000 R 17791 H T TLM1 1000 T 12201.5 V T

TLM2 1000 T 12695 V T

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 24M0G7W 24000 4 27647 0.721 4.8 17 D2 25M8G7W 25800 8 41200 0.641 7.5 19.7

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 1M00F2D 1000 10 22.2 A2 1M00G2D 1000 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) T0001 T0026 D1 1 LB1.doc 68.2 -3.3 16.7 52.3 60.3 -115.3 13.1 T0001 T0026 D2 1 LB2.doc 68.2 -3.3 16.7 52.3 60.3 -115.3 13.1 T0027 T0058 D1 1 LB3.doc 68.2 -3.3 16.7 52.9 58.9 -116.36 13.1 T0027 T0058 D2 1 LB4.doc 68.2 -3.3 16.7 52.9 58.9 -116.36 13.1 TC1 TC2 A1 1 CMD GBL.doc 65.7 1.8 16.8 TC3 TC4 A1 1 CMD OMNI.doc 66 12.1 31 TM1 TM2 A2 1 TLM GBL.doc 24 27 36.7 TM3 TM4 A2 1 TLM OMNI.doc 9 13 41.2

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 85223 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 2450 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3150 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5610 7 0.87 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1050 8 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 92 32 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): 14100 14100 14100 14100 Bus (Watts): (b): (g): (l): (q): 3500 1700 3500 1700 Total (Watts): (c): (h): (m): (r): 17600 15800 17600 15800 Solar Array (Watts): (d): (i): (n): (s): 19500 17500 18500 16500 Depth of Battery (e) (j) (o) (t) Discharge (%): 75 % 75 % 75 % 75 % 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: 2008-01-16 15:17:25
Document Modified: 2008-01-16 15:17:25
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