Attachment Schedule S Tech Data

This document pretains to SES-AMD-20090807-00977 for Amended Filing on a Satellite Earth Station filing.

IBFS_SESAMD2009080700977_730961

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: NIMIQ 5 11/26/2009 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 5/4/2007 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 6/30/2009 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: 8/1/2009 9/30/2009 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) 12.2 G 12.7 G T Broadcasting Satellite Service - Video 12.2 G 12.7 G T Broadcasting Satellite Service - Sound 12.2 G 12.7 G T Broadcasting Satellite Service - Data 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 Cheyenne, WY and Gilbert, AZ uplink sites SATX S 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) RXL R 36.4 28.4 0.15 0.2 30 N SARX 690 8 -105 20 1 RXR R 36.4 28.4 0.15 0.2 30 N SARX 690 8 -105 20 1 TXL T 35.5 29.5 0.15 0.2 30 N SATX 1.8 99.1 55.5 TXR T 35.5 29.5 0.15 0.2 30 N SATX 1.8 99.1 55.5

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) RXL R C -72.7 RXL.gxt RXR R C -72.7 RXR.gxt TXL T C -72.7 TXL.gxt TXR T C -72.7 TXR.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) U01 24000 R 17324 R C T001 134.5 U01 RXR D01 TXR U03 24000 R 17353.16 R C T003 134.5 U03 RXR D03 TXR U05 24000 R 17382.32 R C T005 134.5 U05 RXR D05 TXR U07 24000 R 17411.48 R C T007 134.5 U07 RXR D07 TXR U09 24000 R 17440.64 R C T009 134.5 U09 RXR D09 TXR U11 24000 R 17469.8 R C T011 134.5 U11 RXR D11 TXR U13 24000 R 17498.96 R C T013 134.5 U13 RXR D13 TXR U15 24000 R 17528.12 R C T015 134.5 U15 RXR D15 TXR U17 24000 R 17557.28 R C T017 134.5 U17 RXR D17 TXR U19 24000 R 17586.44 R C T019 134.5 U19 RXR D19 TXR U21 24000 R 17615.6 R C T021 134.5 U21 RXR D21 TXR U23 24000 R 17644.76 R C T023 134.5 U23 RXR D23 TXR U25 24000 R 17673.92 R C T025 134.5 U25 RXR D25 TXR U27 24000 R 17703.08 R C T027 134.5 U27 RXR D27 TXR U29 24000 R 17732.24 R C T029 134.5 U29 RXR D29 TXR U31 24000 R 17761.4 R C T031 134.5 U31 RXR D31 TXR U02 24000 R 17338.58 L C T002 134.5 U02 RXL D02 TXL U04 24000 R 17367.74 L C T004 134.5 U04 RXL D04 TXL U06 24000 R 17396.9 L C T006 134.5 U06 RXL D06 TXL U08 24000 R 17426.06 L C T008 134.5 U08 RXL D08 TXL U10 24000 R 17455.22 L C T010 134.5 U10 RXL D10 TXL U12 24000 R 17484.38 L C T012 134.5 U12 RXL D12 TXL U14 24000 R 17513.54 L C T014 134.5 U14 RXL D14 TXL U16 24000 R 17542.7 L C T016 134.5 U16 RXL D16 TXL U18 24000 R 17571.86 L C T018 134.5 U18 RXL D18 TXL U20 24000 R 17601.02 L C T020 134.5 U20 RXL D20 TXL U22 24000 R 17630.18 L C T022 134.5 U22 RXL D22 TXL U24 24000 R 17659.34 L C T024 134.5 U24 RXL D24 TXL U26 24000 R 17688.5 L C T026 134.5 U26 RXL D26 TXL U28 24000 R 17717.66 L C T028 134.5 U28 RXL D28 TXL

U30 24000 R 17746.82 L C T030 134.5 U30 RXL D30 TXL U32 24000 R 17775.98 L C T032 134.5 U32 RXL D32 TXL D01 24000 T 12224 R C CMD1 TC1 RXR D03 24000 T 12253.16 R C CMD2 TC2 RXL D05 24000 T 12282.32 R C TLM1 TM1 TXR D07 24000 T 12311.48 R C TLM2 TM2 TXL D09 24000 T 12340.64 R C D11 24000 T 12369.8 R C D13 24000 T 12398.96 R C D15 24000 T 12428.12 R C D17 24000 T 12457.28 R C D19 24000 T 12486.44 R C D21 24000 T 12515.6 R C D23 24000 T 12544.76 R C D25 24000 T 12573.92 R C D27 24000 T 12603.08 R C D29 24000 T 12632.24 R C D31 24000 T 12661.4 R C D02 24000 T 12238.58 L C D04 24000 T 12267.74 L C D06 24000 T 12296.9 L C D08 24000 T 12326.06 L C D10 24000 T 12355.22 L C D12 24000 T 12384.38 L C D14 24000 T 12413.54 L C D16 24000 T 12442.7 L C D18 24000 T 12471.86 L C D20 24000 T 12501.02 L C D22 24000 T 12530.18 L C D24 24000 T 12559.34 L C D26 24000 T 12588.5 L C D28 24000 T 12617.66 L C D30 24000 T 12646.82 L C D32 24000 T 12675.98 L C TC1 1000 R 17790 R T TC2 1000 R 17790 L T TM1 1000 T 12695 R T TM2 1000 T 12695 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 27647 0.691 5.7 28 D2 24M0G7W 24000 4 30719 0.768 6.6 28 D3 25M8G7W 25800 8 41200 0.639 7.5 28

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) T001 T032 D1 1 DBS_QPSK1.d 65.7 11.6 19.5 47.5 55.5 13.2 T001 T032 D2 1 DBS_QPSK2.d 65.7 11.6 19.5 47.5 55.5 13.2 T001 T032 D3 1 DBS_8PSK.doc 65.7 11.6 19.5 49.5 55.5 13.2

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: 133438 Allan Park Road S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Allan Park ON N4N 3B8 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 519-371-7490 Remote Control (TT C) Location(s): S14a: Street Address: 5311 Allard Way S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Edmonton AB T6H 5X8 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 780-437-6167

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 1969 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2925 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4794 26.1 0.9546 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1389 8.8 0.8854 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 73.5 6.8 0.8452 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): 7720 7720 7720 7720 Bus (Watts): (b): (g): (l): (q): 1596 1010 1582 958 Total (Watts): (c): (h): (m): (r): 9316 8730 9302 8678 Solar Array (Watts): (d): (i): (n): (s): 12429 11234 10570 9927 Depth of Battery (e) (j) (o) (t) Discharge (%): 71.5 % 71.5 % 71.5 % 71.5 % 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: 2009-08-12 10:59:06
Document Modified: 2009-08-12 10:59:06
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