Attachment Schedule S Tech Data

This document pretains to SAT-AMD-20060120-00006 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2006012000006_477670

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-14 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: 768 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) 17300 M 17800 M R Feeder Link for Broadcasting Satellite Service in FSS 12200 M 12700 M 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: 105.5 W Petition for a Declaratory Ruling allowing BSS services Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be from 105.5W was filed. 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) US_PLUS E CONUS, AK, HI, Puerto Rico, and selected parts of Caribbean, -13 dB contour of beam NG1

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) NG1 T 35.1 22.1 0.13 0 30 N 45 US_PLUS 2.2 77.6 54 NG1 T 35.1 22.1 0.13 0 30 N 45 US_PLUS 2.2 77.6 54 NG1 R 32.1 19.1 27 N 45 US_PLUS 900 2.6 -95.6 20 1 NG1 R 32.1 19.1 27 N 45 US_PLUS 900 2.6 -95.6 20 1 GBL T 4.3 3.3 0.13 0 30 N 45 US_PLUS 1.5 37.1 20 GBL R 4.3 3.3 27 N 45 US_PLUS 790 -24.7 -73.8

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) NG1 T C -105.5 NG1TL_Cpol.gxt -200.8 -170.8 -162.8 -157.8 -156.8 NG1 T X -105.5 NG1TL_Xpol.gxt NG1 T C -105.5 NG1TR_Cpol.gxt -200.8 -170.8 -162.8 -157.8 -156.8 NG1 T X -105.5 NG1TR_Xpol.gxt NG1 R C -105.5 NG1RL_Cpol.gxt NG1 R X -105.5 NG1RL_Xpol.gxt NG1 R C -105.5 NG1RR_Cpol.gxt NG1 R X -105.5 NG1RR_Xpol.gxt GBL T C -105.5 GBLRT_Cpol.gxt -165.8 -164.8 -164.8 -164.8 -164.8 GBL R C -105.5 GBLRR_Cpol.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) T001 24000 T 12217.0 L C TID01 125 R001 NG1RL T001 NG1TL T002 24000 T 12231.58 R C TID02 125 R002 NG1RR T002 NG1TR T003 24000 T 12246.16 L C TID03 125 R003 NG1RL T003 NG1TL T004 24000 T 12260.74 R C TID04 125 R004 NG1RR T004 NG1TR T005 24000 T 12275.32 L C TID05 125 R005 NG1RL T005 NG1TL T006 24000 T 12289.9 R C TID06 125 R006 NG1RR T006 NG1TR T007 24000 T 12304.48 L C TID07 125 R007 NG1RL T007 NG1TL T008 24000 T 12319.06 R C TID08 125 R008 NG1RR T008 NG1TR T009 24000 T 12333.64 L C TID09 125 R009 NG1RL T009 NG1TL T010 24000 T 12348.22 R C TID10 125 R010 NG1RR T010 NG1TR T011 24000 T 12362.8 L C TID11 125 R011 NG1RL T011 NG1TL T012 24000 T 12377.38 R C TID12 125 R012 NG1RR T012 NG1TR T013 24000 T 12391.96 L C TID13 125 R013 NG1RL T013 NG1TL T014 24000 T 12406.54 R C TID14 125 R014 NG1RR T014 NG1TR T015 24000 T 12421.12 L C TID15 125 R015 NG1RL T015 NG1TL T016 24000 T 12435.7 R C TID16 125 R016 NG1RR T016 NG1TR T017 24000 T 12450.28 L C TID17 125 R017 NG1RL T017 NG1TL T018 24000 T 12464.86 R C TID18 125 R018 NG1RR T018 NG1TR T019 24000 T 12479.44 L C TID19 125 R019 NG1RL T019 NG1TL T020 24000 T 12494.02 R C TID20 125 R020 NG1RR T020 NG1TR T021 24000 T 12508.6 L C TID21 125 R021 NG1RL T021 NG1TL T022 24000 T 12523.18 R C TID22 125 R022 NG1RR T022 NG1TR T023 24000 T 12537.76 L C TID23 125 R023 NG1RL T023 NG1TL T024 24000 T 12552.34 R C TID24 125 R024 NG1RR T024 NG1TR T025 24000 T 12566.92 L C TID25 125 R025 NG1RL T025 NG1TL T026 24000 T 12581.5 R C TID26 125 R026 NG1RR T026 NG1TR T027 24000 T 12596.08 L C TID27 125 R027 NG1RL T027 NG1TL T028 24000 T 12610.66 R C TID28 125 R028 NG1RR T028 NG1TR T029 24000 T 12625.24 L C TID29 125 R029 NG1RL T029 NG1TL T030 24000 T 12639.82 R C TID30 125 R030 NG1RR T030 NG1TR

T031 24000 T 12654.4 L C TID31 125 R031 NG1RL T031 NG1TL T032 24000 T 12668.98 R C TID32 125 R032 NG1RR T032 NG1TR R001 24000 R 17317.0 L C TIDTC TC GBLRR R002 24000 R 17331.58 R C TTM1 TM1 GBLRT R003 24000 R 17346.16 L C TTM2 TM2 GBLRT R004 24000 R 17360.74 R C R005 24000 R 17375.32 L C R006 24000 R 17389.9 R C R007 24000 R 17404.48 L C R008 24000 R 17419.06 R C R009 24000 R 17433.64 L C R010 24000 R 17448.22 R C R011 24000 R 17462.8 L C R012 24000 R 17477.38 R C R013 24000 R 17491.96 L C R014 24000 R 17506.54 R C R015 24000 R 17521.12 L C R016 24000 R 17535.7 R C R017 24000 R 17550.28 L C R018 24000 R 17564.86 R C R019 24000 R 17579.44 L C R020 24000 R 17594.02 R C R021 24000 R 17608.6 L C R022 24000 R 17623.18 R C R023 24000 R 17637.76 L C R024 24000 R 17652.34 R C R025 24000 R 17666.92 L C R026 24000 R 17681.5 R C R027 24000 R 17696.08 L C R028 24000 R 17710.66 R C R029 24000 R 17725.24 L C R030 24000 R 17739.82 R C R031 24000 R 17754.4 L C R032 24000 R 17768.98 R C TC 2000 R 17793.5 L T TM1 1000 T 12694.5 L T TM2 1000 T 12698.5 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 27640 0.69 7 20 TM 1M00G9D 1000 9

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) TC 1M50FXW 1500 FDM/FM 1 10

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) TID01 TID32 D1 1 LINK ANALYSI 65 17.3 19 53.5 54 -156.8 13 TIDTC 1 TTC_budgets.xl 64.2 25 25 TTM1 TTM2 TM TTC_budgets.xl 20 20 -164.8 39.5

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): #Error 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 Contol 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

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 2000 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2400 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4400 7.3 0.8964 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1000 3 0.9065 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 71.2 1.9 0.8126 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): 8719 8719 8719 8719 Bus (Watts): (b): (g): (l): (q): 525 436 607 467 Total (Watts): (c): (h): (m): (r): 9244 9155 9326 9186 Solar Array (Watts): (d): (i): (n): (s): 14394 12956 12358 11239 Depth of Battery (e) (j) (o) (t) Discharge (%): 73.9 % % 74.2 % % 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: 2006-01-24 12:02:30
Document Modified: 2006-01-24 12:02:30
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