Attachment Schedule S Tech Data

This document pretains to SES-LFS-20040831-01253 for License to use Foreign Satellite (earth) on a Satellite Earth Station filing.

IBFS_SESLFS2004083101253_406468

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: ANIK-F3 9/1/2006 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 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: 864 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) 14 G 14.5 G R Fixed Satellite Service 11.7 G 12.2 G T Direct to Home in the Fixed 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: 118.7 W Telesat Canada has authorization from Industry Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Canada to operate the satellite at 118.7 ° W.L. Th e N/S Station-Keeping provided (Optional): orbital location is consistent with the Trilateral d. Toward West: Degrees E/W 0.05 Degrees Tolerance: Agreement reached between Canada, Mexico and the g. Westernmost: e. Toward East: 0.05 Degrees United States of America in 1988. 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) SATX S CONUS, Alaska, Hawaii, Puerto Rico SARX E CONUS, Canada

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) TXR T 33.7 28.7 0.13 30 N SATX 1.8 85.9 53 TXLC T 33.7 28.7 0.13 30 N SATX 1.8 85.9 53 RXH R 32.7 28.7 0.13 30 N SARX 825 3.5 -100.5 20 1 RXV R 32.7 23.7 0.13 30 N SARX 825 3.5 -100.5 20 1

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) TXR T C -118 TXRC.gxt TXLC T C -118 TXLC.gxt RXH R C -118 RXHP.gxt RXV R C -118 RXVP.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) UH001 27000 R 14014.75 H C T0001 132.3 UH001 RXHP DR001 TXRC UH003 27000 R 14045.25 H C T0003 132.3 UH003 RXHP DR003 TXRC UH005 27000 R 14075.75 H C T0005 132.3 UH005 RXHP DR005 TXRC UH007 27000 R 14106.25 H C T0007 132.3 UH007 RXHP DR007 TXRC UH009 27000 R 14136.75 H C T0009 132.3 UH009 RXHP DR009 TXRC UH011 27000 R 14167.25 H C T0011 132.3 UH011 RXHP DR011 TXRC UH013 27000 R 14197.75 H C T0013 132.3 UH013 RXHP DR013 TXRC UH015 27000 R 14228.25 H C T0015 132.3 UH015 RXHP DR015 TXRC UH017 27000 R 14258.75 H C T0017 132.3 UH017 RXHP DR017 TXRC UH019 27000 R 14289.25 H C T0019 132.3 UH019 RXHP DR019 TXRC UH021 27000 R 14319.75 H C T0021 132.3 UH021 RXHP DR021 TXRC UH023 27000 R 14350.25 H C T0023 132.3 UH023 RXHP DR023 TXRC UH025 27000 R 14380.75 H C T0025 132.3 UH025 RXHP DR025 TXRC UH027 27000 R 14411.25 H C T0027 132.3 UH027 RXHP DR027 TXRC UH029 27000 R 14441.75 H C T0029 132.3 UH029 RXHP DR029 TXRC UH031 27000 R 14472.25 H C T0031 132.3 UH031 RXHP DR031 TXRC UV002 27000 R 14027.75 V C T0002 132.3 UV002 RXVP DL002 TXLC UV004 27000 R 14058.25 V C T0004 132.3 UV004 RXVP DL004 TXLC UV006 27000 R 14088.75 V C T0006 132.3 UV006 RXVP DL006 TXLC UV008 27000 R 14119.25 V C T0008 132.3 UV008 RXVP DL008 TXLC UV010 27000 R 14149.75 V C T0010 132.3 UV010 RXVP DL010 TXLC UV012 27000 R 14180.25 V C T0012 132.3 UV012 RXVP DL012 TXLC UV014 27000 R 14210.75 V C T0014 132.3 UV014 RXVP DL014 TXLC UV016 27000 R 14241.25 V C T0016 132.3 UV016 RXVP DL016 TXLC UV018 27000 R 14271.75 V C T0018 132.3 UV018 RXVP DL018 TXLC UV020 27000 R 14302.25 V C T0020 132.3 UV020 RXVP DL020 TXLC UV022 27000 R 14332.75 V C T0022 132.3 UV022 RXVP DL022 TXLC UV024 27000 R 14363.25 V C T0024 132.3 UV024 RXVP DL024 TXLC UV026 27000 R 14393.75 V C T0026 132.3 UV026 RXVP DL026 TXLC UV028 27000 R 14424.25 V C T0028 132.3 UV028 RXVP DL028 TXLC

UV030 27000 R 14454.75 V C T0030 132.3 UV030 RXVP DL030 TXLC UV032 27000 R 14485.25 V C T0032 132.3 UV032 RXVP DL032 TXLC DR001 27000 T 11714.75 R C DR003 27000 T 11745.25 R C DR005 27000 T 11775.75 R C DR007 27000 T 11806.25 R C DR009 27000 T 11836.75 R C DR011 27000 T 11867.25 R C DR013 27000 T 11897.75 R C DR015 27000 T 11928.25 R C DR017 27000 T 11958.75 R C DR019 27000 T 11989.25 R C DR021 27000 T 12019.75 R C DR023 27000 T 12050.25 R C DR025 27000 T 12080.75 R C DR027 27000 T 12111.25 R C DR029 27000 T 12141.75 R C DR031 27000 T 12172.25 R C DL002 27000 T 11727.75 L C DL004 27000 T 11758.25 L C DL006 27000 T 11788.75 L C DL008 27000 T 11819.25 L C DL010 27000 T 11849.75 L C DL012 27000 T 11880.25 L C DL014 27000 T 11910.75 L C DL016 27000 T 11941.25 L C DL018 27000 T 11971.75 L C DL020 27000 T 12002.25 L C DL022 27000 T 12032.75 L C DL024 27000 T 12063.25 L C DL026 27000 T 12093.75 L C DL028 27000 T 12124.25 L C DL030 27000 T 12154.75 L C DL032 27000 T 12185.25 L C TC1 1300 R 14496 H T TC2 1300 R 14498 H T TM1 300 T 11701.75 H T TM2 300 T 11701.75 R T TM3 300 T 11702.25 H T

TM4 300 T 11702.25 R 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 0.75 6.1 18.3

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 1M30F9D 1300 1 A2 300KG9D 300 1

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 LB1.doc 0 36.3 5 23.2 48 53 -146.3 15.1

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

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 2280 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2465 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4745 36.2 0.9248 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 900 8.2 0.8615 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 68.9 5.4 0.7967 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): 6855 6855 6855 6855 Bus (Watts): (b): (g): (l): (q): 605 456 605 456 Total (Watts): (c): (h): (m): (r): 7460 7311 7460 7311 Solar Array (Watts): (d): (i): (n): (s): 13476 11684 11946 10401 Depth of Battery (e) (j) (o) (t) Discharge (%): 79.7 % % 79.7 % % 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: 2004-11-24 13:39:27
Document Modified: 2004-11-24 13:39:27
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