Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20041008-00196 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2004100800196_406462

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-117W 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: 64 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: 7360 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) 28.35 G 28.6 G R Fixed Satellite Service 29.25 G 30.0 G R Fixed Satellite Service 18.3 G 18.8 G T Fixed Satellite Service 19.7 G 20.2 G T 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: 117 W This orbital location has been selected because, Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be among other things, it provides high elevation angles N/S Station-Keeping provided (Optional): to all of North America, which is very important for d. Toward West: Degrees E/W 0.05 Degrees Tolerance: satellite services to large numbers of small and g. Westernmost: e. Toward East: 0.05 Degrees inexpensive consumer earth stations. The high 0.05 Degrees h. Easternmost: elevation minimizes the risk of signal blockage due to buildings and foliage, and also minimizes the i. Reason for service are selection (Optional): atmospheric and rain attenuation.

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) NA S CONUS, ALASKA, HAWAII, CANADA, 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) KAR R 45.5 41.5 0.12 0.12 30 N NA 790 16.5 -105 20 1 KARL R 45.5 41.5 0.12 0.12 30 N NA 790 16.5 -105 20 1 KAT T 45.5 41.5 0.12 0.12 30 N NA 2 78.9 64.5 KATL T 45.5 41.5 0.12 0.12 30 N NA 2 78.9 64.5

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) KAR R C -117 KARR.gxt KARL R C -117 KARL.gxt KAT T C -117 KATR.gxt -118 -118 -118 -118 -118 KATL T C -117 KATL.gxt -118 -118 -118 -118 -118

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) U001 115000 R 29312.5 L C T0001 129.5 U001 KARL D0001 KATR U003 115000 R 29437.5 L C T0002 129.5 U003 KARL D0003 KATR U005 115000 R 28412.5 L C T0003 129.5 U005 KARL D0005 KATR U007 115000 R 28537.5 L C T0004 129.5 U007 KARL D0007 KATR U009 115000 R 29562.5 L C T0005 129.5 U009 KARL D0009 KATR U011 115000 R 29687.5 L C T0006 129.5 U011 KARL D0011 KATR U013 115000 R 29812.5 L C T0007 129.5 U013 KARL D0013 KATR U015 115000 R 29937.5 L C T0008 129.5 U015 KARL D0015 KATR U002 115000 R 29312.5 R C T0009 129.5 U002 KARR D0002 KATL U004 115000 R 29437.5 R C T0010 129.5 U004 KARR D0004 KATL U006 115000 R 28412.5 R C T0011 129.5 U006 KARR D0006 KATL U008 115000 R 28537.5 R C T0012 129.5 U008 KARR D0008 KATL U010 115000 R 29562.5 R C T0013 129.5 U010 KARR D0010 KATL U012 115000 R 29687.5 R C T0014 129.5 U012 KARR D0012 KATL U014 115000 R 29812.5 R C T0015 129.5 U014 KARR D0014 KATL U016 115000 R 29937.5 R C T0016 129.5 U016 KARR D0016 KATL D0001 115000 T 18362.5 R C D0003 115000 T 18487.5 R C D0005 115000 T 18612.5 R C D0007 115000 T 18737.5 R C D0009 115000 T 19762.5 R C D0011 115000 T 19887.5 R C D0013 115000 T 20012.5 R C D0015 115000 T 20137.5 R C D0002 115000 T 18362.5 L C D0004 115000 T 18487.5 L C D0006 115000 T 18612.5 L C D0008 115000 T 18737.5 L C D0010 115000 T 19762.5 L C D0012 115000 T 19887.5 L C

D0014 115000 T 20012.5 L C D0016 115000 T 20137.5 L 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) D001 51K2G7W 51.2 4 56 0.691 8.4 20.6 D002 102KG7W 102 4 104 0.691 8.4 20.6 D003 500KG7W 500 4 512 0.691 8.4 20.6 D004 2M00G7W 2000 4 2048 0.691 8.4 20.6 D005 6M80G7W 6800 4 6968 0.691 8.4 20.6 D006 115MG7W 115000 4 117760 0.691 8.4 20.6

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 T0016 D001 1790 64 Ka1 LB.doc 43.9 -15.2 -11.2 16.5 T0001 T0016 D002 1000 125 Ka2 LB.doc 43.9 -8.2 -12.2 16.5 T0001 T0016 D003 200 575 Ka3 LB.doc 43.9 -6 -2 16.5 T0001 T0016 D004 50 2300 Ka4 LB.doc 43.9 0 4 16.5 T0001 T0016 D005 16 7187 Ka5 LB.doc 47.7 1.8 5.8 16.5 T0001 T0016 D006 1 Ka6 LB.doc 60.5 64.5 -118 17.5

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 Remote Control (TT C) Location(s): S14a: Street Address: 801 North American Sky Boulavard 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

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 2400 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3400 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5800 55 0.85 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1400 4 0.83 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 110 5 0.7055 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): 14000 14000 14000 14000 Bus (Watts): (b): (g): (l): (q): 1800 925 1800 925 Total (Watts): (c): (h): (m): (r): 15800 14925 15800 14925 Solar Array (Watts): (d): (i): (n): (s): 18200 17400 16300 15500 Depth of Battery (e) (j) (o) (t) Discharge (%): 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: 2004-11-24 13:36:22
Document Modified: 2004-11-24 13:36:22
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