Attachment Schedule S Tech Data

This document pretains to SES-LFS-20080512-00595 for License to use Foreign Satellite (earth) on a Satellite Earth Station filing.

IBFS_SESLFS2008051200595_641069

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 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 14.000 G 14.003 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: 72.7 W This orbital location is registered at the ITU by the Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Canadian 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) SARX S CONUS SATX S CONUS SATC 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) RXLC R 33.8 29.8 0.12 30 N SARX 590 6.1 -94.7 1 20 RXR R 33.8 29.8 0.12 30 N SARX 590 6.1 -94.7 1 20 TXLC T 35.5 28.8 0.12 30 N SATX 2.3 148 57.2 TXR T 35.5 28.8 0.12 30 N SATX 2.3 148 57.2 TXLC T 35.5 28.8 0.12 30 N SATX 1.8 83 54.7 TXR T 35.5 28.8 0.12 30 N SATX 1.8 83 54.7 GBL R 2 -4 1 30 N SATC 1691 -30.3

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 -72.7 RXLC.gxt TXLC T C -72.7 TXLCH.gxt TXR T C -72.7 TXRCH.gxt RXR R C -72.7 RXRC.gxt TXLC T C -72.7 TXLCM.gxt TXR T C -72.7 TXRCM.gxt GBL R C -72.7

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 129.1 U0001 RXRC D0001 TXRCH U0003 24000 R 17353.16 R C T0003 129.1 U0003 RXRC D0003 TXRCH U0005 24000 R 17382.32 R C T0005 129.1 U0005 RXRC D0005 TXRCH U0007 24000 R 17411.48 R C T0007 129.1 U0007 RXRC D0007 TXRCH U0009 24000 R 17440.64 R C T0009 129.1 U0009 RXRC D0009 TXRCH U0011 24000 R 17469.8 R C T0011 129.1 U0011 RXRC D0011 TXRCH U0013 24000 R 17498.96 R C T0013 129.1 U0013 RXRC D0013 TXRCH U0015 24000 R 17528.12 R C T0015 129.1 U0015 RXRC D0015 TXRCH U0017 24000 R 17557.28 R C T0017 129.1 U0017 RXRC D0017 TXRCH U0019 24000 R 17586.44 R C T0019 129.1 U0019 RXRC D0019 TXRCH U0021 24000 R 17615.6 R C T0021 129.1 U0021 RXRC D0021 TXRCH U0023 24000 R 17644.76 R C T0023 129.1 U0023 RXRC D0023 TXRCH U0025 24000 R 17673.92 R C T0025 129.1 U0025 RXRC D0025 TXRCH U0027 24000 R 17703.08 R C T0027 129.1 U0027 RXRC D0027 TXRCH U0029 24000 R 17732.24 R C T0029 129.1 U0029 RXRC D0029 TXRCH U0031 24000 R 17761.4 R C T0031 129.1 U0031 RXRC D0031 TXRCH U0002 24000 R 17338.58 L C T0002 129.1 U0002 RXLC D0002 TXLCH U0004 24000 R 17367.74 L C T0004 129.1 U0004 RXLC D0004 TXLCH U0006 24000 R 17396.9 L C T0006 129.1 U0006 RXLC D0006 TXLCH U0008 24000 R 17426.06 L C T0008 129.1 U0008 RXLC D0008 TXLCH U0010 24000 R 17455.22 L C T0010 129.1 U0010 RXLC D0010 TXLCH U0012 24000 R 17484.38 L C T0012 129.1 U0012 RXLC D0012 TXLCH U0014 24000 R 17513.54 L C T0014 129.1 U0014 RXLC D0014 TXLCH U0016 24000 R 17542.7 L C T0016 129.1 U0016 RXLC D0016 TXLCH U0018 24000 R 17571.86 L C T0018 129.1 U0018 RXLC D0018 TXLCH U0020 24000 R 17601.02 L C T0020 129.1 U0020 RXLC D0020 TXLCH U0022 24000 R 17630.18 L C T0022 129.1 U0022 RXLC D0022 TXLCH U0024 24000 R 17659.34 L C T0024 129.1 U0024 RXLC D0024 TXLCH U0026 24000 R 17688.5 L C T0026 129.1 U0026 RXLC D0026 TXLCH U0028 24000 R 17717.66 L C T0028 129.1 U0028 RXLC D0028 TXLCH

U0030 24000 R 17746.82 L C T0030 129.1 U0030 RXLC D0030 TXLCH U0032 24000 R 17775.98 L C T0032 129.1 U0032 RXLC D0032 TXLCH D0001 24000 T 12224 R C C001 CR001 RXLC D0003 24000 T 12253.16 R C T001 TM001 TXLCH D0005 24000 T 12282.32 R C T002 TM002 TXLCH D0007 24000 T 12311.48 R C T0033 126.6 U0001 RXRC D0001 TXRCM D0009 24000 T 12340.64 R C T0035 126.6 U0003 RXRC D0003 TXRCM D0011 24000 T 12369.8 R C T0037 126.6 U0005 RXRC D0005 TXRCM D0013 24000 T 12398.96 R C T0039 126.6 U0007 RXRC D0007 TXRCM D0015 24000 T 12428.12 R C T0041 126.6 U0009 RXRC D0009 TXRCM D0017 24000 T 12457.28 R C T0043 126.6 U0011 RXRC D0011 TXRCM D0019 24000 T 12486.44 R C T0045 126.6 U0013 RXRC D0013 TXRCM D0021 24000 T 12515.6 R C T0047 126.6 U0015 RXRC D0015 TXRCM D0023 24000 T 12544.76 R C T0049 126.6 U0017 RXRC D0017 TXRCM D0025 24000 T 12573.92 R C T0051 126.6 U0019 RXRC D0019 TXRCM D0027 24000 T 12603.08 R C T0053 126.6 U0021 RXRC D0021 TXRCM D0029 24000 T 12632.24 R C T0055 126.6 U0023 RXRC D0023 TXRCM D0031 24000 T 12661.4 R C T0057 126.6 U0025 RXRC D0025 TXRCM D0002 24000 T 12238.58 L C T0059 126.6 U0027 RXRC D0027 TXRCM D0004 24000 T 12267.74 L C T0061 126.6 U0029 RXRC D0029 TXRCM D0006 24000 T 12296.9 L C T0063 126.6 U0031 RXRC D0031 TXRCM D0008 24000 T 12326.06 L C T0034 126.6 U0002 RXLC D0002 TXLCM D0010 24000 T 12355.22 L C T0036 126.6 U0004 RXLC D0004 TXLCM D0012 24000 T 12384.38 L C T0038 126.6 U0006 RXLC D0006 TXLCM D0014 24000 T 12413.54 L C T0040 126.6 U0008 RXLC D0008 TXLCM D0016 24000 T 12442.7 L C T0042 126.6 U0010 RXLC D0010 TXLCM D0018 24000 T 12471.86 L C T0044 126.6 U0012 RXLC D0012 TXLCM D0020 24000 T 12501.02 L C T0046 126.6 U0014 RXLC D0014 TXLCM D0022 24000 T 12530.18 L C T0048 126.6 U0016 RXLC D0016 TXLCM D0024 24000 T 12559.34 L C T0050 126.6 U0018 RXLC D0018 TXLCM D0026 24000 T 12588.5 L C T0052 126.6 U0020 RXLC D0020 TXLCM D0028 24000 T 12617.66 L C T0054 126.6 U0022 RXLC D0022 TXLCM D0030 24000 T 12646.82 L C T0056 126.6 U0024 RXLC D0024 TXLCM D0032 24000 T 12675.98 L C T0058 126.6 U0026 RXLC D0026 TXLCM CR001 1000 R 17305 L T T0060 126.6 U0028 RXLC D0028 TXLCM TM001 800 T 12203 L T T0062 126.6 U0030 RXLC D0030 TXLCM TM002 800 T 12204 L T T0064 126.6 U0032 RXLC D0032 TXLCM CR002 800 R 14001 R T T003 TM001 TXLCM CR003 800 R 14002.5 R T T004 TM002 TXLCM

C002 CR002 GBLU C003 CR003 GBLU

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) T0001 T0032 D1 1 DBS_QPSK1_ 65.7 -0.2 19.5 51 57.1 13.2 C001 C001 CMD 1 CMD LB.doc 65 -14.5 9.5 T001 T002 TLM 1 TLM LB.doc 10 16 36.7 T0001 T0032 D2 1 DBS_QPSK2_ 65.7 -0.2 19.5 51 57.1 13.2 T0001 T0032 D3 1 DBS_8PSK_H 65.7 -0.2 19.5 51 57.1 13.2 T0033 T0064 D1 1 DBS_QPSK1_ 65.7 -0.2 19.5 49 54.6 13.2 T0033 T0064 D2 1 DBS_QPSK2_ 65.7 -0.2 19.5 49 54.6 13.2 T0033 T0064 D3 1 DBS_8PSK_M 65.7 -0.2 19.5 49 54.6 13.2 C002 C003 CMD 1 CMD_LB_14G 65 15 18

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 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: 2008-05-13 12:57:48
Document Modified: 2008-05-13 12:57:48
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