Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20080910-00173 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2008091000173_663807

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: AMC-22 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: 28 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: 960.4 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) 17.300 G 17.800 G T Broadcasting Satellite Service - Video 24.75 G 25.25 G R Feeder Link for Broadcasting Satellite Service in FSS 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: 67.5 W Availability of spectrum 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) C-UL S CONUS, -8 dB contour C-DL S CONUS, -6 dB contour M-UL S Mexico, -10 dB contour M-DL S Mexico, -10 dB contour B-UL S Brazil, -10 dB contour B-DL S Brazil, -6 dB contour S-UL S South Americal (excluding Brazil), -10 dB contour S-DL S South America (excluding Brazil), -10 dB contour

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) RCL R 33.9 25.9 0.15 0 30 Y C-UL 600 6 -93 20 1 RCR R 33.9 25.9 0.15 0 30 Y C-UL 60 6 -93 20 1 TCL T 36.4 28.4 0.15 0 30 Y C-DL 1.5 200 59.4 TCR T 36.4 28.4 0.15 0 30 Y C-DL 1.5 200 59.4 RML R 33.9 25.9 0.15 0 30 Y M-UL 600 6 -93 20 1 RMR R 33.9 25.9 0.15 0 30 Y M-UL 600 6 -93 20 1 TML T 37.1 29.1 0.15 0 30 Y M-DL 2.2 170 59.4 TMR T 37.1 29.1 0.15 0 30 Y M-DL 2.2 170 59.4 RBL R 33.9 27.9 0.15 0 30 Y B-UL 600 6 -93 20 1 RBR R 33.9 27.9 0.15 0 30 Y B-UL 600 6 -93 20 1 TBL T 35.2 29.2 0.15 0 30 Y B-DL 1.2 210 58.5 TBR T 35.2 29.2 0.15 0 30 Y B-DL 1.2 210 58.5 RSL R 34.6 27.3 0.15 0 30 Y S-UL 600 6.8 -93 20 1 RSR R 34.6 27.3 0.15 0 30 Y S-UL 600 6.8 -93 20 1 TSL T 34.1 26.1 0.15 0 30 Y S-DL 1.3 210 57.3 TSR T 34.1 26.1 0.15 0 30 Y S-DL 1.3 210 57.3

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) TCL T C -67.5 CON_DL_LHPC.gxt -126.5 -128 -126.5 -126 -123 TCR T C -67.5 CON_DL_RHPC.gxt -126.5 -128 -126.5 -126 -123 TML T C -67.5 MEX_DL_LHPC.gxt -159 -154 -149 -144 -139 TMR T C -67.5 MEX_DL_RHPC.gxt -159 -154 -149 -144 -139 TBL T C -67.5 BRAZ_DL_LHCP.gxt -189.9 -185.9 -183.9 -181.9 -179.9 TBR T C -67.5 BRAZ_DL_RHCP.gxt -189.9 -185.9 -183.9 -181.9 -179.9 TSL T C -67.5 SPANISH_DL_LHPC.gxt -161.1 -158.6 -156.1 -154.1 -151.1 TSR T C -67.5 SPANISH_DL_RHPC.gxt -161.1 -158.6 -156.1 -154.1 -151.1 RCL R C -67.5 CON_UL_LHPC.gxt RCR R C -67.5 CON_UL_RHPC.gxt RML R C -67.5 MEX_UL_LHPC.gxt RMR R C -67.5 MEX_UL_RHPC.gxt RBL R C -67.5 BRAZ_UL_LHCP.gxt RBR R C -67.5 BRAZ_UL_RHCP.gxt RSL R C -67.5 RSR R C -67.5

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) NAU1 31000 R 24769.15 L C CON01 120 NAU1 RCL NAD1 TCR NAU2 31000 R 24786.30 R C CON02 120 NAU2 RCR NAD2 TCL NAU3 31000 R 24803.45 L C CON03 120 NAU3 RCL NAD3 TCR NAU4 31000 R 24820.60 R C CON04 120 NAU4 RCR NAD4 TCL NAU5 31000 R 24837.75 L C CON05 120 NAU5 RCL NAD5 TCR NAU6 31000 R 24854.90 R C CON06 120 NAU6 RCR NAD6 TCL NAU7 31000 R 24872.05 L C CON07 120 NAU7 RCL NAD7 TCR NAU8 31000 R 24889.20 R C CON08 120 NAU8 RCR NAD8 TCL NAU9 31000 R 24906.35 L C CON09 120 NAU9 RCL NAD9 TCR NAU10 31000 R 24923.50 R C CON10 120 NAU10 RCR NAD10 TCL NAU11 31000 R 24940.65 L C CON11 120 NAU11 RCL NAD11 TCR NAU12 31000 R 24957.80 R C CON12 120 NAU12 RCR NAD12 TCL NAU13 31000 R 24974.95 L C CON13 120 NAU13 RCL NAD13 TCR NAU14 31000 R 24992.10 R C CON14 120 NAU14 RCR NAD14 TCL NAU15 31000 R 25009.25 L C CON15 120 NAU15 RCL NAD15 TCR NAU16 31000 R 25026.40 R C CON16 120 NAU16 RCR NAD16 TCL NAU17 31000 R 25043.55 L C CON17 120 NAU17 RCL NAD17 TCR NAU18 31000 R 25060.70 R C CON18 120 NAU18 RCR NAD18 TCL NAU19 31000 R 25077.85 L C CON19 120 NAU19 RCL NAD19 TCR NAU20 31000 R 25095.00 R C CON20 120 NAU20 RCR NAD20 TCL NAU21 31000 R 25112.15 L C CON21 120 NAU21 RCL NAD21 TCR NAU22 31000 R 25129.30 R C CON22 120 NAU22 RCR NAD22 TCL NAU23 31000 R 25146.45 L C MEX01 120 NAU23 RML NAD23 TMR NAU24 31000 R 25163.60 R C MEXO2 120 NAU24 RMR NAD24 TML NAU25 31000 R 25180.75 L C MEX03 120 NAU25 RML NAD25 TMR NAU26 31000 R 25197.90 R C MEX04 120 NAU26 RMR NAD26 TML NAU27 31000 R 25215.05 L C MEX05 120 NAU27 RML NAD27 TMR NAU28 31000 R 25232.20 R C MEX06 120 NAU28 RMR NAD28 TML NAD1 31000 T 17319.15 R C BRZ01 120 SAU1 RBL SAD1 TBR NAD2 31000 T 17336.30 L C BRZ02 120 SAU2 RBR SAD2 TBL

NAD3 31000 T 17353.45 R C BRZ03 120 SAU3 RBL SAD3 TBR NAD4 31000 T 17370.60 L C BRZ04 120 SAU4 RBR SAD4 TBL NAD5 31000 T 17387.75 R C BRZ05 120 SAU5 RBL SAD5 TBR NAD6 31000 T 17404.90 L C BRZ06 120 SAU6 RBR SAD6 TBL NAD7 31000 T 17422.05 R C BRZ07 120 SAU7 RBL SAD7 TBR NAD8 31000 T 17439.20 L C BRZ08 120 SAU8 RBR SAD8 TBL NAD9 31000 T 17456.35 R C BRZ09 120 SAU9 RBL SAD9 TBR NAD10 31000 T 17473.50 L C BRZ10 120 SAU10 RBR SAD10 TBL NAD11 31000 T 17490.65 R C BRZ11 120 SAU11 RBL SAD11 TBR NAD12 31000 T 17507.80 L C BRZ12 120 SAU12 RBR SAD12 TBL NAD13 31000 T 17524.95 R C BRZ13 120 SAU13 RBL SAD13 TBR NAD14 31000 T 17542.10 L C BRZ14 120 SAU14 RBR SAD14 TBL NAD15 31000 T 17559.25 R C SPN01 120 SAU15 RSL SAD15 TSR NAD16 31000 T 17576.40 L C SPN02 120 SAU16 RSR SAD16 TSL NAD17 31000 T 17593.55 R C SPN03 120 SAU17 RSL SAD17 TSR NAD18 31000 T 17610.70 L C SPN04 120 SAU18 RSR SAD18 TSL NAD19 31000 T 17627.85 R C SPN05 120 SAU19 RSL SAD19 TSR NAD20 31000 T 17645.00 L C SPN06 120 SAU20 RSR SAD20 TSL NAD21 31000 T 17662.15 R C SPN07 120 SAU21 RSL SAD21 TSR NAD22 31000 T 17679.30 L C SPN08 120 SAU22 RSR SAD22 TSL NAD23 31000 T 17696.45 R C SPN09 120 SAU23 RSL SAD23 TSR NAD24 31000 T 17713.60 L C SPN10 120 SAU24 RSR SAD24 TSL NAD25 31000 T 17730.75 R C SPN11 120 SAU25 RSL SAD25 TSR NAD26 31000 T 17747.90 L C SPN12 120 SAU26 RSR SAD26 TSL NAD27 31000 T 17765.05 R C SPN13 120 SAU27 RSL SAD27 TSR NAD28 31000 T 17782.20 L C SPN14 120 SAU28 RSR SAD28 TSL SAU1 31000 R 24769.15 L C CMD1 TC1 RCL SAU2 31000 R 24786.30 R C CMD2 TC2 RCR SAU3 31000 R 24803.45 L C TLMA TLM1 TCR SAU4 31000 R 24820.60 R C TLMB TLM2 TCL SAU5 31000 R 24837.75 L C SAU6 31000 R 24854.90 R C SAU7 31000 R 24872.05 L C SAU8 31000 R 24889.20 R C SAU9 31000 R 24906.35 L C SAU10 31000 R 24923.50 R C SAU11 31000 R 24940.65 L C SAU12 31000 R 24957.80 R C SAU13 31000 R 24974.95 L C

SAU14 31000 R 24992.10 R C SAU15 31000 R 25009.25 L C SAU16 31000 R 25026.40 R C SAU17 31000 R 25043.55 L C SAU18 31000 R 25060.70 R C SAU19 31000 R 25077.85 L C SAU20 31000 R 25095.00 R C SAU21 31000 R 25112.15 L C SAU22 31000 R 25129.30 R C SAU23 31000 R 25146.45 L C SAU24 31000 R 25163.60 R C SAU25 31000 R 25180.75 L C SAU26 31000 R 25197.90 R C SAU27 31000 R 25215.05 L C SAU28 31000 R 25232.20 R C SAD1 31000 T 17319.15 R C SAD2 31000 T 17336.30 L C SAD3 31000 T 17353.45 R C SAD4 31000 T 17370.60 L C SAD5 31000 T 17387.75 R C SAD6 31000 T 17404.90 L C SAD7 31000 T 17422.05 R C SAD8 31000 T 17439.20 L C SAD9 31000 T 17456.35 R C SAD10 31000 T 17473.50 L C SAD11 31000 T 17490.65 R C SAD12 31000 T 17507.80 L C SAD13 31000 T 17524.95 R C SAD14 31000 T 17542.10 L C SAD15 31000 T 17559.25 R C SAD16 31000 T 17576.40 L C SAD17 31000 T 17593.55 R C SAD18 31000 T 17610.70 L C SAD19 31000 T 17627.85 R C SAD20 31000 T 17645.00 L C SAD21 31000 T 17662.15 R C SAD22 31000 T 17679.30 L C SAD23 31000 T 17696.45 R C SAD24 31000 T 17713.60 L C

SAD25 31000 T 17730.75 R C SAD26 31000 T 17747.90 L C SAD27 31000 T 17765.05 R C SAD28 31000 T 17782.20 L C TC1 1000 R 24752 L T TC2 1000 R 24753 R T TLM1 1000 T 17302 R T TLM2 1000 T 17303 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) A 31M0G7W 31000 4 39000 0.75 4.4 18 B 31M0G7W 31000 4 45500 0.875 6.2 18 C 31M0G7W 31000 8 46800 0.6 6.1 18

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) D 800KF9D 800 10 18 E 300KF9D 300 9 18

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) CON01 CON22 A 1 link budgets.xls 68 10 16 51.4 59.4 -119 16 BRZ01 BRZ14 A 1 link budgets.xls 68 10 16 52.5 58.5 -119.9 16 SPN01 SPN14 A 1 link budgets.xls 68 10 16 50.3 57.3 -121.1 16 CON01 CON22 B 1 link budgets.xls 68 10 16 51.4 59.4 -119 16 CON01 CON22 C 1 link budgets.xls 68 10 16 51.4 59.4 -119 16 MEX01 MEX06 C 1 link budgets.xls 68 10 16 51.4 59.4 -119 16 CMD1 CMD2 D 1 TT_C budets.xl 65 -10 8

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: Woodbine TT&C S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Mt. Airy MD 21771 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 410-549-4300 E7169 Remote Control (TT C) Location(s): S14a: Street Address: Vernon Valley Spacecraft S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Sussex NJ 07461 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 973-823-6000 WB81 Remote Control (TT C) Location(s): S14a: Street Address: S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):

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 2755 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 5985 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5870 2.2 0.82 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1050 2 0.91 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 120 5.5 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): 11600 11600 11600 11600 Bus (Watts): (b): (g): (l): (q): 2350 1430 2280 1320 Total (Watts): (c): (h): (m): (r): 13950 13030 13880 12920 Solar Array (Watts): (d): (i): (n): (s): 19380 17280 15300 14200 Depth of Battery (e) (j) (o) (t) Discharge (%): 60 % % 64 % % 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 10:14:52
Document Modified: 2008-09-12 10:14:52
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