Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20080910-00186 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2008091000186_663905

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: TELSTAR RDBS-1 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: 26 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: 624 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) 24.75 G 25.15 G R Feeder Link for Broadcasting Satellite Service in FSS 17.3 G 17.7 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: 70 W Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be 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) CANCON 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) RX1R R 36 30 0.12 0.1 25 N CANCON 631 8 -95 20 1 RX1L R 36 30 0.12 0.1 25 N CANCON 631 8 -95 20 1 TX1R T 36 28 0.12 0.1 25 N CANCON 2 251 60 TX1L T 36 28 0.12 0.1 25 N CANCON 2 251 60 TTC R 4 0 0.12 0.1 30 N GBL 3160 -31 TTCT T 4 0 0.12 0.1 30 N GBL 3 50 21

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) RX1R R C -70 RX1R.gxt RX1L R C -70 RX1L.gxt TX1R T C -70 TX1R.gxt -123.1 -122.7 -122.5 -122.4 -122 TX1L T C -70 TX1L.gxt -123.1 -122.7 -122.5 -122.4 -122 TTC R C -70 TTCR_OMNI.gxt TTCT T C -70 TTCT_OMNI.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) 1R 24000 R 24772 R C TP01 132.4 1R RX1R 1T TX1R 2R 24000 R 24786.58 L C TP02 132.4 2R RX1L 2T TX1L 3R 24000 R 24801.16 R C TP03 132.4 3R RX1R 3T TX1R 4R 24000 R 24815.74 L C TP04 132.4 4R RX1L 4T TX1L 5R 24000 R 24830.32 R C TO05 132.4 5R RX1R 5T TX1R 6R 24000 R 24844.9 L C TP06 132.4 6R RX1L 6T TX1L 7R 24000 R 24859.48 R C TP07 132.4 7R RX1R 7T TX1R 8R 24000 R 24874.06 L C TP08 132.4 8R RX1L 8T TX1L 9R 24000 R 24888.64 R C TP09 132.4 9R RX1R 9T TX1R 10R 24000 R 24903.22 L C TP10 132.4 10R RX1L 10T TX1L 11R 24000 R 24917.8 R C TP11 132.4 11R RX1R 11T TX1R 12R 24000 R 24932.38 L C TP12 132.4 12R RX1L 12T TX1L 13R 24000 R 24946.96 R C TP13 132.4 13R RX1R 13T TX1R 14R 24000 R 24961.54 L C TP14 132.4 14R RX1L 14T TX1L 15R 24000 R 24976.12 R C TP15 132.4 15R RX1R 15T TX1R 16R 24000 R 24990.7 L C TP16 132.4 16R RX1L 16T TX1L 17R 24000 R 25005.28 R C TP17 132.4 17R RX1R 17T TX1R 18R 24000 R 25019.86 L C TP18 132.4 18R RX1L 18T TX1L 19R 24000 R 25034.44 R C TP19 132.4 19R RX1R 19T TX1R 20R 24000 R 25049.02 L C TP20 132.4 20R RX1L 20T TX1L 21R 24000 R 25063.6 R C TP21 132.4 21R RX1R 21T TX1R 22R 24000 R 25078.18 L C TP22 132.4 22R RX1L 22T TX1L 23R 24000 R 25092.76 R C TP23 132.4 23R RX1R 23T TX1R 24R 24000 R 25107.34 L C TP24 132.4 24R RX1L 24T TX1L 25R 24000 R 25121.92 R C TP25 132.4 25R RX1R 25T TX1R 26R 24000 R 25136.5 L C TP26 132.4 26R RX1L 26T TX1L 1T 24000 T 17322 R C CMDA CMD1 TTCR 2T 24000 T 17336.58 L C CMDB CMD2 TTCR 3T 24000 T 17351.16 R C TLMA TLM1 TTCT 4T 24000 T 17365.74 L C TLMB TLM2 TTCT

5T 24000 T 17380.32 R C 6T 24000 T 17394.9 L C 7T 24000 T 17409.48 R C 8T 24000 T 17424.06 L C 9T 24000 T 17438.64 R C 10T 24000 T 17453.22 L C 11T 24000 T 17467.8 R C 12T 24000 T 17482.38 L C 13T 24000 T 17496.96 R C 14T 24000 T 17511.54 L C 15T 24000 T 17526.12 R C 16T 24000 T 17540.7 L C 17T 24000 T 17555.28 R C 18T 24000 T 17569.86 L C 19T 24000 T 17584.44 R C 20T 24000 T 17599.02 L C 21T 24000 T 17613.6 R C 22T 24000 T 17628.18 L C 23T 24000 T 17642.76 R C 24T 24000 T 17657.34 L C 25T 24000 T 17671.92 R C 26T 24000 T 17686.5 L C CMD1 1000 R 24751.5 R T CMD2 1000 R 24752.5 L T TLM1 200 T 17301.5 R T TLM2 200 T 17302.5 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) DT1 24M0G7W 24000 4 27647 0.721 4.5 20 DT2 12M0G7W 12000 4 13823 0.721 4.5 20 DT3 4M00G7W 4000 4 4608 0.721 4.5 20

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 1M00F9D 1000 1 10 20 TLM 200KF1D 200 1 10 20

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) TP01 TP26 DT1 1 Table LB1.xls 65.56 -2.7 17.3 52 60 -115.3 13.3 CMDA CMDB CMD 1 Table CMD.doc 67.23 -7.49 25.7 TLMA TLMB TLM 1 Table TLM.doc 11 21 39.4

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: 1601 Telesat Court S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Ottawa ON K1B 5P4 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): +1-613-748-0123

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 2850 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3650 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6500 3 0.85 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1205 3 0.84 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 120 6 0.72 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): 18000 18000 18000 18000 Bus (Watts): (b): (g): (l): (q): 3500 2000 3500 2000 Total (Watts): (c): (h): (m): (r): 21500 20000 21500 20000 Solar Array (Watts): (d): (i): (n): (s): 24000 22100 22600 20900 Depth of Battery (e) (j) (o) (t) Discharge (%): 75 % 75 % 75 % 75 % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: X 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 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: 2008-09-12 15:00:21
Document Modified: 2008-09-12 15:00:21
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