Attachment Schedule S Tech Data

This document pretains to SAT-PPL-20041004-00194 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2004100400194_401282

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 F2 10/31/2004 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: 53 0 MHz d. Estimated Launch Date: h. Total Transponder Bandwidth (no. transponders x Bandwidth) l. Orbit Type: Mark all boxes that apply: 7/17/2004 5632 MHz GSO NGSO 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) 18.3 G 18.8 G T Fixed Satellite Service 19.7 G 20.2 G T Fixed Satellite Service 28.35 G 28.6 G R Fixed Satellite Service 29.25 G 30 G R 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: 111.1 W The authority to operate Ka-band at 111.1 W.L. was Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be granted by Canadian Administration to Telesat Canada N/S Station-Keeping provided (Optional): on June 23, 1999. Under this application, we are d. Toward West: Degrees Degrees E/W 0.05 Tolerance: seeking authorization to provide services to the US g. Westernmost: e. Toward East: 0.05 Degrees territories in the identified bands. Anik F2 will be 0.05 Degrees h. Easternmost: replacing Anik E2-R satellite system. 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) 1 S Throughout CONUS and 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 Flux Density (Y/N) Value Size (dB) (dBW) Temp (k) Pt. (dBW/m2) 5 R 46.5 42 0.07 30 N 1 510 19.5 -104.5 17 1 5 T 46.5 42 0.07 N 1 2 19.5 64 9 R 46.5 42 0.07 30 N 1 510 19.5 -104.5 17 1 9 T 46.5 42 0.07 N 1 2 19.5 64 24 R 46.5 42 0.07 30 N 1 510 19.5 -104.5 17 1 24 T 46.5 42 0.07 N 1 2 19.5 64 28 R 46.5 42 0.07 30 N 1 510 19.5 -104.5 17 1 28 T 46.5 42 0.07 N 1 2 19.5 64 30 R 46.5 42 0.07 30 N 1 510 19.5 -104.5 17 1 30 T 46.5 42 0.07 N 1 2 19.5 64 44 R 46.5 42 0.07 30 N 1 510 19.5 -104.5 17 1 44 T 46.5 42 0.07 N 1 2 19.5 64 14 R 46.5 42 0.07 30 N 1 510 19.5 -112.5 17 1 14 T 46.5 42 0.07 N 1 5 16.5 61 45 R 46.5 42 0.07 30 N 1 510 19.5 -112.5 17 1 45 T 46.5 42 0.07 N 1 2 19.5 64

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) 5 R C -111.1 F2_Beam5_Rx.gxt 5 T C -111.1 F2_Beam5_Tx.gxt -142.9 -141.8 -138.8 -132.9 -129.3 9 R C -111.1 F2_Beam9_Rx.gxt 9 T C -111.1 F2_Beam9_Tx.gxt -148.1 -148.1 -138.1 -132.1 -129.3 24 R C -111.1 F2_Beam24_Rx.gxt 24 T C -111.1 F2_Beam24_Tx.gxt -149 -149 -149 -149 -129 28 R C -111.1 F2_Beam28_Rx.gxt 28 T C -111.1 F2_Beam28_Tx.gxt -142.1 -142.1 -142.1 -140.3 -129.2 30 R C -111.1 F2_Beam30_Rx.gxt 30 T C -111.1 F2_Beam30_Tx.gxt -148.9 -148.9 -148.9 -148.9 -128.9 44 R C -111.1 F2_Beam44_Rx.gxt 44 T C -111.1 F2_Beam44_Tx.gxt -148.8 -148.8 -148.8 -148.8 -128.8 14 R C -111.1 F2_Beam14_Rx.gxt 14 T C -111.1 F2_Beam14_Tx.gxt -139.1 -139.1 -139.1 -139.1 -119.1 45 R C -111.1 F2_Beam45_Rx.gxt 45 T C -111.1 F2_Beam45_Tx.gxt -142 -142 -142 -142 -122

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) (c) (d) Center (e) (f) TTC (a) (b) Receive Band Transmit Band Channel Assigned T/R Frequency Polarization or Comm Transponder Transponder (c) Channel (d) Beam (e) Channel (f) Beam ID No. Bandwidth Mode (MHz) (H, V, L, R) Channel ID Gain (dB) No. ID No. (kHz) (T or C) F1 56000 R 28382 L C T1 115 F8 5 F8 5 F1 56000 T 19732 L C T2 115 F7 9 F7 9 F2 56000 R 28444 L C T3 115 F4 24 F4 24 F2 56000 T 19794 L C T4 115 F3 44 F3 44 F3 56000 R 28506 L C T5 115 F5 28 F5 28 F3 56000 T 19856 L C T6 115 F4 30 F4 30 F4 56000 R 28568 L C T7 115 F3 30 F3 14 F4 56000 T 19918 L C T8 115 F8 44 F8 45 F5 56000 R 29282 L C T9 132 R4 5 R500 5 F5 56000 T 19982 L C T10 132 R4 14 R500 30 F6 56000 R 29344 L C T11 132 R11 45 R500 44 F6 56000 T 20044 L C F7 56000 R 29406 L C F7 56000 T 20106 L C F8 56000 R 29468 L C F8 56000 T 20168 L C R1 36000 R 29525 R C R2 36000 R 29566 R C R3 36000 R 29607 R C R4 36000 R 29648 R C R5 36000 R 29689 R C R6 36000 R 29730 R C R7 36000 R 29771 R C R8 36000 R 29812 R C R9 36000 R 29853 R C R10 36000 R 29894 R C R11 36000 R 29935 R C R12 36000 R 29976 R C R500 500000 T 18525 R C

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) 1 25M2G7W 25200 4 19740 0.5 5.2 17.4 2 1M60G7W 1600 4 1280 0.5 5.6 17.8

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. Bandwidth per Carrier NTSC, Weighting SCPC/FM Preemphasis, Objective Objective Companded Baseband Baseband Modulation ID (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) T1 T8 1 2 28000 65.6 -3.1 13.9 60.5 77.5 -118.8 17.5 T9 T11 2 21 1700 44.6 4.5 4.5 47.1 47.1 -128.8 37.7

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 N4N3B8 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 519-371-7490

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 3508 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2139 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5948 47.9 0.768 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 316 8.2 0.895 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 60 7.3 0.685 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): 13900 13900 13100 13100 Bus (Watts): (b): (g): (l): (q): 3060 2140 3050 2130 Total (Watts): (c): (h): (m): (r): 16960 16040 16150 15230 Solar Array (Watts): (d): (i): (n): (s): 18770 16370 17130 15510 Depth of Battery (e) (j) (o) (t) Discharge (%): 80.2 % 17 % 75.7 % 17.3 % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: YES NO 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 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? 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: 2004-10-15 12:17:00
Document Modified: 2004-10-15 12:17:00
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