Attachment Schedule S Tech Data

This document pretains to SES-MFS-20080617-00805 for Modification w/ Foreign Satellite (earth station) on a Satellite Earth Station filing.

IBFS_SESMFS2008061700805_648736

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-2 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: 16 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: 384 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 5.920 G 5.925 G R Space Operations Service 3.69 G 3.7 G T Space Operations Service 6.425 G 6.430 G R Space Operations 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: 77.15 W This nominal orbital location is registered at the ITU by Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be the Mexican administration. 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) SAC S Partial CONUS SAM S Mexico SAGBL S Visible Earth SARX S Partial CONUS

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) RXC R 31.4 25.4 0.12 0.2 30 N SARX 513 4.3 -96 18 1.5 TXC T 36.1 26.1 0.12 0.2 30 N SAC 2.1 80.2 55.1 TXM T 36.1 26.1 0.12 0.2 30 N SAM 2.1 80.2 55.1 GBL R 22 16.4 1 30 N SAGBL 2818 -12.5 GBL T 18 12.4 1 30 N SAGBL 4.7 0.5 10.3 OMN R 2 -3 1 30 N SAGBL 1500 -29.8 OMN T 3 -3 1 30 N SAGBL 1.9 3.9 8.9

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) RXC R C -77.15 RXC.gxt TXC T C -77.15 TXC.gxt TXM T C -77.15 TXM.gxt GBL R C -77.15 GBLU.gxt GBL T C -77.15 GBLD.gxt OMN R C -77.15 OMN T C -77.15

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) U0002 24000 R 17338.58 L C T0001 118 U0002 RXC D0002 TXC U0004 24000 R 17367.74 L C T0002 118 U0004 RXC D0004 TXM U0006 24000 R 17396.9 L C T0003 118 U0006 RXC D0006 TXC U0008 24000 R 17426.06 L C T0004 118 U0008 RXC D0008 TXM U0010 24000 R 17455.22 L C T0005 118 U0010 RXC D0010 TXC U0012 24000 R 17484.38 L C T0006 118 U0012 RXC D0012 TXM U0014 24000 R 17513.54 L C T0007 118 U0014 RXC D0014 TXC U0016 24000 R 17542.7 L C T0008 118 U0016 RXC D0016 TXM U0018 24000 R 17571.86 L C T0009 118 U0018 RXC D0018 TXC U0020 24000 R 17601.02 L C T0010 118 U0020 RXC D0020 TXM U0022 24000 R 17630.18 L C T0011 118 U0022 RXC D0022 TXC U0024 24000 R 17659.34 L C T0012 118 U0024 RXC D0024 TXM U0026 24000 R 17688.5 L C T0013 118 U0026 RXC D0026 TXC U0028 24000 R 17717.66 L C T0014 118 U0028 RXC D0028 TXM U0030 24000 R 17746.82 L C T0015 118 U0030 RXC D0030 TXC U0032 24000 R 17775.98 L C T0016 118 U0032 RXC D0032 TXM CR002 800 R 6426.5 H T T001 TM001 GBLD D0002 24000 T 12238.58 L C T002 TM002 GBLD D0004 24000 T 12267.74 L C C001 CR001 GBLU D0006 24000 T 12296.9 L C T003 TM001 OMND D0008 24000 T 12326.06 L C T004 TM002 OMND D0010 24000 T 12355.22 L C C002 CR002 OMNU D0012 24000 T 12384.38 L C D0014 24000 T 12413.54 L C D0016 24000 T 12442.7 L C D0018 24000 T 12471.86 L C D0020 24000 T 12501.02 L C D0022 24000 T 12530.18 L C D0024 24000 T 12559.34 L C D0026 24000 T 12588.5 L C

D0028 24000 T 12617.66 L C D0030 24000 T 12646.82 L C D0032 24000 T 12675.98 L C CR001 800 R 5923.5 H T TM001 800 T 3698.5 H T TM002 800 T 3699.5 H 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 0.691 5.7 17.9 D2 24M0G7W 24000 4 30719 0.768 6.6 18.8 D3 25M8G7W 25800 8 41200 0.639 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) CMD 800KG2D 800 1 9 21.2 TLM 800KG2D 800 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) C001 C001 CMD 1 CMD LB_horn. 53.1 11.7 15.7 T001 T002 TLM 1 TLM LB_horn.d 5 10.6 27.2 T0001 T0016 D1 1 DBS_CONUS_ 65.7 -0.2 19.5 45.1 55.1 13.2 T0001 T0016 D2 1 DBS_CONUS_ 65.7 -0.2 19.5 45.1 55.1 13.2 T0001 T0016 D3 1 DBS_CONUS_ 65.7 -0.2 19.5 45.1 55.1 13.2 T0001 T0016 D1 1 DBS_MEXICO_ 65.7 -0.2 19.5 45.1 55.1 13.2 T0001 T0016 D2 1 DBS_MEXICO_ 65.7 -0.2 19.5 45.1 55.1 13.2 T0001 T0016 D3 1 DBS_MEXICO_ 65.7 -0.2 19.5 45.1 55.1 13.2 C002 C002 CMD 1 CMD LB_omni. 53.1 22.7 25.7 T003 T004 TLM 1 TLM LB_omni.d 3.9 8.9 27.2

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 1324 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1541 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2865 23.8 0.92 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 422 4.6 0.82 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 51.3 7.1 0.75 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): 3978 3878 3978 3878 Bus (Watts): (b): (g): (l): (q): 1075 617 1075 617 Total (Watts): (c): (h): (m): (r): 5053 4495 5053 4495 Solar Array (Watts): (d): (i): (n): (s): 7126 6307 5257 4910 Depth of Battery (e) (j) (o) (t) Discharge (%): 68.8 % % 68.8 % % 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: 2008-06-19 09:41:45
Document Modified: 2008-06-19 09:41:45
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC