Attachment Sched S Tech Report

This document pretains to SAT-MOD-20130227-00026 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2013022700026_989942

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-6 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 f. Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode 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: 96.2 W The ECHOSTAR-6 satellite will operate pursuant to an Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be authorization from Bermuda's Department of N/S Station-Keeping provided (Optional): Telecommunications. The ITU Region 2 BSS Plan has d. Toward West: Degrees E/W 0.05 Degrees Tolerance: assigned the 96.2W.L. location to Bermuda. g. Westernmost: e. Toward East: 0.05 Degrees 0.5 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 Angle (o) Other Plane (Seconds) Node (Deg.) (Degrees) 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 -4 dB contour of beams RXLC and RXRC SA2 S Bermuda and parts of the Caribbean

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) Input (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB) ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Losses Output Max. System Max. Saturation (Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step (dBi) (dBi) (dB) Power (W) EIRP Noice Gain Pt. Flux Density (Y/N) Value Size (dBW) Temp (k) (db/K) (dBW/m2) RXLC R 33.8 29.8 0.12 30 N SA1 590 6.1 -94.7 1 20 RXR R 33.8 29.8 0.12 30 N SA1 590 6.1 -94.7 1 20 TXLC T 35.5 30.5 0.12 30 N SA2 1.8 83.2 54.7 TXRC T 35.5 30.5 0.12 30 N SA2 1.8 83.2 54.7

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 -96.2 RXLC.gxt RXR R C -96.2 RXRC.gxt TXLC T C -96.2 TXLC.gxt TXRC T C -96.2 TXRC.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 (T ID Gain (dB) No. ID No. or C) U0001 24000 R 17324 R C T0001 126.6 U0001 RXRC D0001 TXRC U0003 24000 R 17353.16 R C T0003 126.6 U0003 RXRC D0003 TXRC U0005 24000 R 17382.32 R C T0005 126.6 U0005 RXRC D0005 TXRC U0007 24000 R 17411.48 R C T0007 126.6 U0007 RXRC D0007 TXRC U0009 24000 R 17440.64 R C T0009 126.6 U0009 RXRC D0009 TXRC U0011 24000 R 17469.8 R C T0011 126.6 U0011 RXRC D0011 TXRC U0013 24000 R 17498.96 R C T0013 126.6 U0013 RXRC D0013 TXRC U0015 24000 R 17528.12 R C T0015 126.6 U0015 RXRC D0015 TXRC U0017 24000 R 17557.28 R C T0017 126.6 U0017 RXRC D0017 TXRC U0019 24000 R 17586.44 R C T0019 126.6 U0019 RXRC D0019 TXRC U0021 24000 R 17615.6 R C T0021 126.6 U0021 RXRC D0021 TXRC U0023 24000 R 17644.76 R C T0023 126.6 U0023 RXRC D0023 TXRC U0025 24000 R 17673.92 R C T0025 126.6 U0025 RXRC D0025 TXRC U0027 24000 R 17703.08 R C T0027 126.6 U0027 RXRC D0027 TXRC U0029 24000 R 17732.24 R C T0029 126.6 U0029 RXRC D0029 TXRC U0031 24000 R 17761.4 R C T0031 126.6 U0031 RXRC D0031 TXRC U0002 24000 R 17338.58 L C T0002 126.6 U0002 RXLC D0002 TXLC U0004 24000 R 17367.74 L C T0004 126.6 U0004 RXLC D0004 TXLC U0006 24000 R 17396.9 L C T0006 126.6 U0006 RXLC D0006 TXLC U0008 24000 R 17426.06 L C T0008 126.6 U0008 RXLC D0008 TXLC U0010 24000 R 17455.22 L C T0010 126.6 U0010 RXLC D0010 TXLC U0012 24000 R 17484.38 L C T0012 126.6 U0012 RXLC D0012 TXLC U0014 24000 R 17513.54 L C T0014 126.6 U0014 RXLC D0014 TXLC U0016 24000 R 17542.7 L C T0016 126.6 U0016 RXLC D0016 TXLC U0018 24000 R 17571.86 L C T0018 126.6 U0018 RXLC D0018 TXLC U0020 24000 R 17601.02 L C T0020 126.6 U0020 RXLC D0020 TXLC U0022 24000 R 17630.18 L C T0022 126.6 U0022 RXLC D0022 TXLC U0024 24000 R 17659.34 L C T0024 126.6 U0024 RXLC D0024 TXLC U0026 24000 R 17688.5 L C T0026 126.6 U0026 RXLC D0026 TXLC U0028 24000 R 17717.66 L C T0028 126.6 U0028 RXLC D0028 TXLC

U0030 24000 R 17746.82 L C T0030 126.6 U0030 RXLC D0030 TXLC U0032 24000 R 17775.98 L C T0032 126.6 U0032 RXLC D0032 TXLC D0001 24000 T 12224 R C CMD01 CMD01 RXLC D0003 24000 T 12253.16 R C TLM01 TLM01 TXLC D0005 24000 T 12282.32 R C TLM02 TLM02 TXLC D0007 24000 T 12311.48 R C D0009 24000 T 12340.64 R C D0011 24000 T 12369.8 R C D0013 24000 T 12398.96 R C D0015 24000 T 12428.12 R C D0017 24000 T 12457.28 R C D0019 24000 T 12486.44 R C D0021 24000 T 12515.6 R C D0023 24000 T 12544.76 R C D0025 24000 T 12573.92 R C D0027 24000 T 12603.08 R C D0029 24000 T 12632.24 R C D0031 24000 T 12661.4 R 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 CMD01 1000 R 17305 L T TLM01 800 T 12203 L T TLM02 800 T 12204 L 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 19218 0.48 1.7 13.9 D2 24M0G7W 24000 4 28828 0.721 4.8 17

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 1 9 21.2 A2 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. Power (o)Assoc. Transponder (kHz) No.) Bandwidth (Table S11) (Table S12) Stn. Max. Power (dBW) Flux Density Stn Rec. (a) Start (b) End (kHz) Antenna (dBW/m2/Hz) G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dB/K) T0001 T0032 D1 1 LB1.doc 65.7 6.3 19.3 44.8 49.8 14.3 T0001 T0032 D2 1 LB2.doc 65.7 6.3 19.3 44.8 49.8 17.6 CMD01 CMD01 A1 1 CMD LB.doc 62.2 -7.7 12.3 TLM01 TLM02 A2 1 TLM LB.doc 10 16 39.8

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: 335 Dish Drive S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Quickburg Shenandoah VA 22847 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 540-477-5004 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 1480.6 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2219.8 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3700.4 31.1 0.83 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 548.2 8 0.84 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 68.9 8.8 0.7 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): 6807 6826 6807 6826 Bus (Watts): (b): (g): (l): (q): 2212 1222 2212 1222 Total (Watts): (c): (h): (m): (r): 9019 8048 9019 8048 Solar Array (Watts): (d): (i): (n): (s): 11274 10110 7865 7130 Depth of Battery (e) (j) (o) (t) Discharge (%): 74.9 % % 74.9 % % 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: 2013-03-15 11:24:01
Document Modified: 2013-03-15 11:24:01
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