Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20050819-00163 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2005081900163_451796

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-6 11/20/2000 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 8/1/1998 20 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 9/20/2000 28 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: 10/22/2000 1152 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) 13.75 G 14.00 G R Fixed Satellite Service 13.75 G 14.00 G R Direct to Home in the Fixed Fixed Satellite Service 11.45 G 11.70 G T Fixed Satellite Service 11.45 G 11.70 G T Direct to Home in the Fixed Fixed Satellite Service 14.00 G 14.50 G R Direct to Home in the Fixed Fixed Satellite Service 14.00 G 14.50 G R Fixed Satellite Service 11.70 G 12.20 G T Direct to Home in the Fixed Fixed Satellite Service 11.70 G 12.20 G T 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: 72 No change to the existing orbital location is proposed. 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: 72 W e. Toward East: 0.05 Degrees 0.1 Degrees h. Easternmost: 72 W 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) NAM E -15 dB gain contours of the NAH and NAV beams STEER E -15 dB gain contours of the STH and STV beams

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) NAH T 33.5 18.5 0.15 0 30 Y 0 NAM 1.9 71 52 NAV T 33.5 18.5 0.15 0 30 Y 90 NAM 1.9 71 52 NAH R 33.8 18.8 0.15 0 30 Y 0 NAM 603 6 -100 18 1 NAV R 33.8 18.8 0.15 0 30 Y 90 NAM 603 6 -100 18 1 STH T 33.2 18.2 0.15 0 30 Y 0 STEER 1.6 76.1 52 STV T 33.2 18.2 0.15 0 30 Y 90 STEER 1.6 76.1 52 STH R 33.5 18.5 0.15 0 30 Y 0 STEER 603 5.7 -100.3 18 1 STV R 33.5 18.5 0.15 0 30 Y 90 STEER 603 5.7 -100.3 18 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) NAH T C AMC6 NAM Beam Xmit.gxt -151 -151 -151 -151 -151 NAV T C AMC6 NAM Beam Xmit.gxt -151 -151 -151 -151 -151 NAH R C AMC6 NAM Beam Rx.gxt NAV R C AMC6 NAM Beam Rx.gxt STH T C AMC6 Steer Beam Xmit.gxt -154 -154 -154 -154 -153 STV T C AMC6 Steer Beam Xmit.gxt -154 -154 -154 -154 -153 STH R C AMC6 Steer Beam Rx.gxt STV R C AMC6 Steer Beam Rx.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) ST025 72000 T 11575 V C SS025 128.2 ST125 STH ST025 STV ST026 72000 T 11575 H C SS026 128.2 ST126 STV ST026 STH ST027 72000 T 11655 V C SS027 128.2 ST127 STH ST027 STV ST028 72000 T 11655 H C SS028 128.2 ST128 STV ST028 STH NA025 72000 T 11575 V C NN025 124.5 NA125 NAH NA025 NAV NA026 72000 T 11575 H C NN026 124.5 NA126 NAV NA026 NAH NA027 72000 T 11655 V C NN027 124.5 NA127 NAH NA027 NAV NA028 72000 T 11655 H C NN028 124.5 NA128 NAV NA028 NAH ST125 72000 R 13875 H C SN025 124.5 ST125 STH NA025 NAV ST126 72000 R 13875 V C SN026 124.5 ST126 STV NA026 NAH ST127 72000 R 13955 H C SN027 124.5 ST127 STH NA027 NAV ST128 72000 R 13955 V C SN028 124.5 ST128 STV NA028 NAH NA125 72000 R 13875 H C NS025 128.2 NA125 NAH ST025 STV NA126 72000 R 13875 V C NS026 128.2 NA126 NAV ST026 STH NA127 72000 R 13955 H C NS027 128.2 NA127 NAH ST027 STV NA128 72000 R 13955 V C NS028 128.2 NA128 NAV ST028 STH ST101 36000 R 14020 H C SN001 124.5 ST101 STH NA001 NAV ST103 36000 R 14060 H C SN003 124.5 ST103 STH NA003 NAV ST105 36000 R 14100 H C SN005 124.5 ST105 STH NA005 NAV ST107 36000 R 14140 H C SN007 124.5 ST107 STH NA007 NAV ST109 36000 R 14180 H C SN009 124.5 ST109 STH NA009 NAV ST111 36000 R 14220 H C SN011 124.5 ST111 STH NA011 NAV ST113 36000 R 14260 H C SN013 124.5 ST113 STH NA013 NAV ST115 36000 R 14300 H C SN015 124.5 ST115 STH NA015 NAV ST117 36000 R 14340 H C SN017 124.5 ST117 STH NA017 NAV ST119 36000 R 14380 H C SN019 124.5 ST119 STH NA019 NAV ST121 36000 R 14420 H C SN021 124.5 ST121 STH NA021 NAV ST123 36000 R 14460 H C SN023 124.5 ST123 STH NA023 NAV ST102 36000 R 14040 V C SN002 124.5 ST102 STV NA002 NAH ST104 36000 R 14080 V C SN004 124.5 ST104 STV NA004 NAH

ST106 36000 R 14120 V C SN006 124.5 ST106 STV NA006 NAH ST108 36000 R 14160 V C SN008 124.5 ST108 STV NA008 NAH ST110 36000 R 14200 V C SN010 124.5 ST110 STV NA010 NAH ST112 36000 R 14240 V C SN012 124.5 ST112 STV NA012 NAH ST114 36000 R 14280 V C SN014 124.5 ST114 STV NA014 NAH ST116 36000 R 14320 V C SN016 124.5 ST116 STV NA016 NAH ST118 36000 R 14360 V C SN018 124.5 ST118 STV NA018 NAH ST120 36000 R 14400 V C SN020 124.5 ST120 STV NA020 NAH ST122 36000 R 14440 V C SN022 124.5 ST122 STV NA022 NAH ST124 36000 R 14480 V C SN024 124.5 ST124 STV NA024 NAH NA001 36000 T 11720 V C NA003 36000 T 11760 V C NA005 36000 T 11800 V C NA007 36000 T 11840 V C NA009 36000 T 11880 V C NA011 36000 T 11920 V C NA013 36000 T 11960 V C NA015 36000 T 12000 V C NA017 36000 T 12040 V C NA019 36000 T 12080 V C NA021 36000 T 12120 V C NA023 36000 T 12160 V C NA002 36000 T 11740 H C NA004 36000 T 11780 H C NA006 36000 T 11820 H C NA008 36000 T 11860 H C NA010 36000 T 11900 H C NA012 36000 T 11940 H C NA014 36000 T 11980 H C NA016 36000 T 12020 H C NA018 36000 T 12060 H C NA020 36000 T 12100 H C NA022 36000 T 12140 H C NA024 36000 T 12180 H 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) A 1M60G1W 1600 4 1544 0.75 7.5 16 B 6M95G1W 6950 4 8000 0.75 7.5 16 C 32M4G7D 32400 4 30000 0.75 4.2 18 D 32M4G7D 32400 4 30000 0.75 3.3 18 E 36M0G7W 36000 4 40000 0.75 7.5 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)

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) NS025 NS028 A 23 1600 AMC6 Link Bud 46.6 53.6 63.6 28.5 32.5 -159.7 24.6 NS025 NS028 B 5 6950 AMC6 Link Bud 52.8 61 71 35.7 39.5 -158.4 24.6 NS025 NS028 C 1 AMC6 Link Bud 60 76 78 50 52 -149.3 10 NS025 NS028 E 1 AMC6 Link Bud 57.2 75 77.7 50 52 -150.3 17.1 SN001 SN024 A 23 1600 AMC6 Link Bud 46.6 48 51.6 28.5 32.5 -159.7 24.6 SN001 SN024 B 5 6950 AMC6 Link Bud 52.8 55 57.8 35.7 39.5 -158.4 24.6 SN001 SN024 D 1 AMC6 Link Bud 46.6 65.1 63.1 45 47 -154.3 38.4

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: 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 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: Grand Junction S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Grand Junction CO 81505 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 970-241-8300 E890537 Remote Control (TT C) Location(s): S14a: Street Address: South Mountain S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Somis CA 93066 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 805-386-4195 E940156

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 1769 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2066 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3835 2 0.75 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 732 2 0.87 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 35.25 6.25 0.66 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): 6915 6915 6931 6931 Bus (Watts): (b): (g): (l): (q): 1410 740 1431 757 Total (Watts): (c): (h): (m): (r): 8325 7655 8362 7688 Solar Array (Watts): (d): (i): (n): (s): 10191 9040 9430 8445 Depth of Battery (e) (j) (o) (t) Discharge (%): 80 % 80 % 80 % 80 % 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: 2005-08-26 10:16:31
Document Modified: 2005-08-26 10:16:31
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