Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20040917-00184 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2004091700184_397037

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-157W 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 d. Estimated Launch Date: 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) 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 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: 157 W Winning bidder for 157W orbital location in DBS Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Auction No. 52. 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) SARX S Defined by the -3 dB contour. CONUS. SATX S Defined by the -4 dB contour. CONUS, Alaska, Hawaii, Mexico.

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) RXLC R 37.6 34.6 0.12 30 N SARX 915 8 -95 1 20 RXR R 37.6 34.6 0.12 30 N SARX 915 8 -95 1 20 TXLC T 34.6 30.6 0.12 30 N SATX 1.8 198.2 57.4 TXR T 34.6 30.6 0.12 30 N SATX 1.8 198.2 57.4

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) RXLC R C -157 RXLC.gxt TXLC T C -157 TXLC.gxt TXR T C -157 TXRC.gxt RXR R C -157 RXRC.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 17324 R C T0001 123.7 U0001 RXRC D0001 TXLC U0003 24000 R 17353.16 R C T0003 123.7 U0003 RXRC D0003 TXLC U0005 24000 R 17382.32 R C T0005 123.7 U0005 RXRC D0005 TXLC U0007 24000 R 17411.48 R C T0007 123.7 U0007 RXRC D0007 TXLC U0009 24000 R 17440.64 R C T0009 123.7 U0009 RXRC D0009 TXLC U0011 24000 R 17469.8 R C T0011 123.7 U0011 RXRC D0011 TXLC U0013 24000 R 17498.96 R C T0013 123.7 U0013 RXRC D0013 TXLC U0015 24000 R 17528.12 R C T0015 123.7 U0015 RXRC D0015 TXLC U0017 24000 R 17557.28 R C T0017 123.7 U0017 RXRC D0017 TXLC U0019 24000 R 17586.44 R C T0019 123.7 U0019 RXRC D0019 TXLC U0021 24000 R 17615.6 R C T0021 123.7 U0021 RXRC D0021 TXLC U0023 24000 R 17644.76 R C T0023 123.7 U0023 RXRC D0023 TXLC U0025 24000 R 17673.92 R C T0025 123.7 U0025 RXRC D0025 TXLC U0027 24000 R 17703.08 R C T0027 123.7 U0027 RXRC D0027 TXLC U0029 24000 R 17732.24 R C T0029 123.7 U0029 RXRC D0029 TXLC U0031 24000 R 17761.4 R C T0031 123.7 U0031 RXRC D0031 TXLC U0002 24000 R 17338.58 L C T0002 123.7 U0002 RXLC D0002 TXRC U0004 24000 R 17367.74 L C T0004 123.7 U0004 RXLC D0004 TXRC U0006 24000 R 17396.9 L C T0006 123.7 U0006 RXLC D0006 TXRC U0008 24000 R 17426.06 L C T0008 123.7 U0008 RXLC D0008 TXRC U0010 24000 R 17455.22 L C T0010 123.7 U0010 RXLC D0010 TXRC U0012 24000 R 17484.38 L C T0012 123.7 U0012 RXLC D0012 TXRC U0014 24000 R 17513.54 L C T0014 123.7 U0014 RXLC D0014 TXRC U0016 24000 R 17542.7 L C T0016 123.7 U0016 RXLC D0016 TXRC U0018 24000 R 17571.86 L C T0018 123.7 U0018 RXLC D0018 TXRC U0020 24000 R 17601.02 L C T0020 123.7 U0020 RXLC D0020 TXRC U0022 24000 R 17630.18 L C T0022 123.7 U0022 RXLC D0022 TXRC U0024 24000 R 17659.34 L C T0024 123.7 U0024 RXLC D0024 TXRC U0026 24000 R 17688.5 L C T0026 123.7 U0026 RXLC D0026 TXRC U0028 24000 R 17717.66 L C T0028 123.7 U0028 RXLC D0028 TXRC

U0030 24000 R 17746.82 L C T0030 123.7 U0030 RXLC D0030 TXRC U0032 24000 R 17775.98 L C T0032 123.7 U0032 RXLC D0032 TXRC D0001 24000 T 12224 L C D0003 24000 T 12253.16 L C D0005 24000 T 12282.32 L C D0007 24000 T 12311.48 L C D0009 24000 T 12340.64 L C D0011 24000 T 12369.8 L C D0013 24000 T 12398.96 L C D0015 24000 T 12428.12 L C D0017 24000 T 12457.28 L C D0019 24000 T 12486.44 L C D0021 24000 T 12515.6 L C D0023 24000 T 12544.76 L C D0025 24000 T 12573.92 L C D0027 24000 T 12603.08 L C D0029 24000 T 12632.24 L C D0031 24000 T 12661.4 L C D0002 24000 T 12238.58 R C D0004 24000 T 12267.74 R C D0006 24000 T 12296.9 R C D0008 24000 T 12326.06 R C D0010 24000 T 12355.22 R C D0012 24000 T 12384.38 R C D0014 24000 T 12413.54 R C D0016 24000 T 12442.7 R C D0018 24000 T 12471.86 R C D0020 24000 T 12501.02 R C D0022 24000 T 12530.18 R C D0024 24000 T 12559.34 R C D0026 24000 T 12588.5 R C D0028 24000 T 12617.66 R C D0030 24000 T 12646.82 R C D0032 24000 T 12675.98 R C

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 0.691 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)

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 T0032 D1 1 LB1.doc 0 65 3.2 21.8 50.6 57.4 12.7

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 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) 633-5227 E980005 Remote Control (TT C) Location(s): S14a: Street Address: 801 North American Sky Boulevard 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): (307) 633-5227 E020306

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 2000 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2200 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4200 47.1 0.87 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1500 8 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 91.2 5 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): 10500 10500 10500 10500 Bus (Watts): (b): (g): (l): (q): 2000 1111 2000 1111 Total (Watts): (c): (h): (m): (r): 12500 11611 12500 11611 Solar Array (Watts): (d): (i): (n): (s): 15500 13439 13740 12090 Depth of Battery (e) (j) (o) (t) Discharge (%): 76 % % 76 % % 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: 2004-09-24 07:13:04
Document Modified: 2004-09-24 07:13:04
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