Attachment Sched S Tech Report

This document pretains to SAT-AMD-20100514-00101 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2010051400101_817403

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: MSAT-2 1/1/1996 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 10 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 1 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: 4/7/1995 29 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) 14.0005 G 14.0005 G R Satellite Command 1631.5 M 1660.5 M R Mobile-Satellite Service 1530 M 1559 M T Mobile-Satellite Service 13.0 G 13.25 G R Feeder Link for Mobile Satellite Service in FSS 11.701 G 11.701 G T Satellite Telemetery 11.7005 G 11.7005 G T Satellite Telemetry 10.75 G 10.95 G T Feeder Link for Mobile Satellite Service in FSS 14.4495 G 14.4495 G R Satellite Command 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: 103.3 W MSAT-2 currently operates at 101.3 degrees west Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be longitude. SkyTerra requests authority to relocate it N/S Station-Keeping provided (Optional): temporarily to 103.3 degrees west longitude prior to d. Toward West: Degrees E/W 0.05 Degrees Tolerance: the launch of SkyTerra 1 as described in the g. Westernmost: e. Toward East: 0.05 Degrees application narrative. 6 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) LA1 S MSAT-103.3 CONUS S CONUS, Alaska, Canada, and as shown LA2 S MSAT-103.3 HI Svc Are Hawaii KU1 S MSAT-2 30B 103.3 KU CONUS, Alaska, Canada, Hawaii and as shown OMNI S MSAT-2 103.3 Omni SA GLOBAL

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) LE1 T 34 28 0.12 0.2 20 N LA1 1 500 57.3 LR1 R 34 28 0.12 0.2 20 N LA1 600 3.2 7.5 2.5 LE2 T 34 28 0.12 0.2 20 N LA1 1 500 57.3 LR2 R 34 28 0.12 0.2 20 N LA1 600 3.2 7.5 2.5 LE3 T 34 28 0.12 0.2 20 N LA1 1 500 57.3 LR3 R 34 28 0.12 0.2 20 N LA1 600 3.2 7.5 2.5 LE4 T 34 28 0.12 0.2 20 N LA1 1 500 57.3 LR4 R 34 28 0.12 0.2 20 N LA1 600 3.2 7.5 2.5 LE5 T 30 24 0.12 0.2 20 N LA1 1 500 57.3 LR5 R 30 24 0.12 0.2 20 N LA1 600 -0.8 7.5 2.5 LE6 T 30 24 0.12 0.2 20 N LA2 1 500 57.3 LR6 R 30 24 0.12 0.2 20 N LA2 600 -0.8 7.5 2.5 KU1E T 29.2 23.2 0.12 0.2 20 N 90 KU1 1 6 36.2 KU1 R 29.2 23.2 0.12 0.2 20 N 0 KU1 600 -3.6 7.5 2.5 OMNI T 2 2 0.12 0.2 12 N 90 OMNI 1 0.16 7.4 OMNI R 2 2 0.12 0.2 9N 0 OMNI 600 -8 1 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) LE1 T C -103.3 MSAT-2-Tx-East 103.3W.gxt -134.2 -134 -133.9 -133.8 -133.7 LR1 R C -103.3 MSAT-2-Rx-East 103.3W.gxt LE2 T C -103.3 MSAT-2-Tx-Central 103.3W.gxt -134.2 -134 -133.9 -133.8 -133.7 LR2 R C -103.3 MSAT-2-Rx-Central 103.3W.gxt LE3 T C -103.3 MSAT-2-Tx-Mountain 103.3W.gxt -134.2 -134 -133.9 -133.8 -133.7 LR3 R C -103.3 MSAT-2-Rx-Mountain 103.3W.gxt LE4 T C -103.3 MSAT-2-Tx-West 103.3W.gxt -134.2 -134 -133.9 -133.8 -133.7 LR4 R C -103.3 MSAT-2-Rx-West 103.3W.gxt LE5 T C -103.3 MSAT-2-Tx-South 103.3.gxt -134.2 -134 -133.9 -133.8 -133.7 LR5 R C -103.3 MSAT-2-Rx-South 103.3.gxt LE6 T C -103.3 MSAT-2-Tx-AH 103.3W.gxt -134.2 -134 -133.9 -133.8 -133.7 LR6 R C -103.3 MSAT-2-Rx-AH 103.3W.gxt KU1E T C -103.3 MSAT-2 30B KU1E 103.3W.gxt -159.6 -159.4 -159.3 -159.2 -159.1 KU1 R C -103.3 MSAT-2 30B KU1R 103.3W.gxt OMNI T C -103.3 MSAT-2-OMNI-E 103.3W.gxt -209 -209 -209 -209 -209 OMNI R C -101.3 MSAT-2-OMNI-R 103.3W.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) KUD 200000 T 10850 V C FWD1 123.3 KUU KU1R LD LE1 KUU 200000 R 13125 H C FWD2 123.3 KUU KU1R LD LE2 LD 29000 T 1544.5 R C FWD3 123.3 KUU KU1R LD LE3 LU 29000 R 1646.0 R C FWD4 123.3 KUU KU1R LD LE4 THG1 1000 T 11701 H T FWD5 123.3 KUU KU1R LD LE5 TOMN1 1000 T 11701 V T FWD6 123.3 KUU KU1R LD LE6 COMH 100 R 14000.5 H T RET1 122 LU LR1 KUD KU1E COMNI 100 R 14449.5 V T RET2 122 LU LR2 KUD KU1E THG2 1000 T 117005 H T RET3 122 LU LR3 KUD KU1E TOMN2 1000 T 117005 V T RET4 122 LU LR4 KUD KU1E BEAC1 1 T 10753.5 V C RET5 122 LU LR5 KUD KU1E BEAC2 1T 10751 V C RET6 122 LU LR5 KUD KU1E CMDOM COMNI OMNIR CMDHG COMHG KU1R TELO1 TOMN1 OMNIE TELO2 TOMN2 OMNIE TELH1 THG1 KU1E TELH2 THG2 KU1E AFC1 BEAC1 KU1E AFC2 BEAC2 KU1E

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) CW1 1K00N 1 1 9.8 22 GCS 6K00G1D 6 4 0 9.9 22.1 MMS 5K00G1D 5 2 600 0.5 0 4.2 16.4 DATAF 270KG1D 300 4 270 0.5 0 4 16 DATA1 168KG1D 168 2 2.637 -5 7.2 DATA2 42K0G1D 42 2 2.637 -11 1.2 QPSKV 6K00G1D 6 4 9.9 22.1

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) TELE 138GX 100 PM 1 5 17 CMD 700KF9D 1000 SCPC/FM 1 25 17

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) FWD1 FWD6 DATA1 1 MSAT DATA1 61 -5.5 -1.5 30 34 -144.7 -25.3 FWD1 FWD6 DATA2 1 MSAT DATA2 61 -7.5 -3.5 28 32 -140.7 -25.3 RET1 RET6 QPSKV 1 MSAT QPSK V 8 5 9.2 4.6 8.8 -155.5 36.5 RET1 RET6 DATA1 1 MSAT DATA1 3 4.52 8.52 -0.88 3.12 -175.6 36.5 RET1 RET6 DATA2 1 MSAT DATA2 3 4.52 8.52 -0.88 3.12 -169.6 36.5 FWD1 FWD6 CW1 1 MSAT CW Carr 61 -7.5 -5.5 28 30 -132.5 -16 FWD1 FWD6 GCS 1 MSAT GCS EO 61 -5.5 -1.5 30 34 -130.3 -16 FWD1 FWD6 MMS 1 MSAT MMS Ca 61 -15.5 -11 20 24.5 -139 -20 FWD1 FWD6 DATAF 1 MSAT DATAF 61 5.5 9.5 41 45 -136.3 -10 RET1 RET6 CW1 1 MSAT CW Carr 8 3.5 9.5 3.1 9.1 -153.4 36.5 RET1 RET6 GCS 1 MSAT GCS EO 8 5 12.5 6.5 12.1 -152.2 36.5 RET1 RET6 MMS 1 MSAT MMS Ca 4 -4.5 1.5 -8.9 -2.9 -166.4 36.5 RET1 RET6 DATAF 1 MSAT DATAF 14 18.3 24.4 23.9 30 -151.3 36.5 CMDOM CMDOM CMD 1 Telemetry and 59.5 24.5 27.5 CMDHG CMDHG CMD 1 Telemetry and 59.5 9.5 12.5 TELO1 TELO2 TELEM 1 Telemetry and 7.5 7.5 -169 35 TELH1 TELH2 TELEM 1 Telemetry and 17.5 17.5 -159 35 AFC1 AFC2 CW1 1 MSAT Beacon 10 10 -152.5 36 FWD1 FWD6 QPSKV 1 MSAT QPSK V 61 -7.5 -4.5 28 31 -131.7 -16

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 K1B 1B9 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 888-835-3728 x3315 Remote Control (TT C) Location(s): S14a: Street Address: 10802 Parkridge Boulevard S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Reston Fairfax VA 20191 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 703-390-2700 E930124

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 1326 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1670 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2996 69 0.904 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1666 53 0.906 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 32.9 69 0.819 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): 2516 2516 2535 2535 Bus (Watts): (b): (g): (l): (q): 718 475 718 475 Total (Watts): (c): (h): (m): (r): 3234 3234 3234 3234 Solar Array (Watts): (d): (i): (n): (s): 4073 3695 3357 3126 Depth of Battery (e) (j) (o) (t) Discharge (%): 72.1 % 0 % 72.1 % 6 % 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? X 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? 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: 2010-05-17 16:54:03
Document Modified: 2010-05-17 16:54:03
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