Attachment Schedule S Tech Data

This document pretains to SAT-RPL-20051118-00233 for Replacement Application on a Satellite Space Stations filing.

IBFS_SATRPL2005111800233_486462

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: GALAXY 16 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 48 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: 1728 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) 5925 M 6425 M R Fixed Satellite Service 3700 M 4200 M T Fixed Satellite Service 14000 M 14500 M R Fixed Satellite Service 11700 M 12200 M 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: 99 W REPLACES GALAXY-4R 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) 1 S CONTINENTAL USA, HAWAII, ALASKA, PUERTO RICO, PORTIONS OF CANADA AND MEXICO 2 S 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) CHU R 31 25 0.16 0.16 27.5 Y 01 528 3.8 -106.5 31 1 CVU R 31 25 0.16 0.16 27.5 Y 90 1 528 3.8 -106.5 31 1 CHD T 29.2 25.2 0.16 0.16 30 Y 0 1 2 28.2 43.7 CVD T 29.2 25.2 0.16 0.16 30 Y 90 1 2 28.2 43.7 KHU R 33.3 27.3 0.16 0.16 27 Y 0 1 519 6.1 -104.1 31 1 KVU R 33.3 27.3 0.16 0.16 27 Y 90 1 519 6.1 -104.1 31 1 KHD T 32.8 26.8 0.16 0.16 30 Y 0 1 2 81.3 51.9 KVD T 32.8 26.8 0.16 0.16 30 Y 90 1 2 81.3 51.9 UPC T 32.8 26.8 0.16 0.16 30 Y 0 1 0.02 16.3 UPC T 32.8 26.8 0.16 0.16 30 Y 90 1 0.02 16.3 OMN R 5.4 -0.6 0.16 0.16 18.5 Y 2 9235 -34.3 -97.8 OMN T 5.6 -3.9 0.16 0.16 20 Y 2 6.8 9.3 15.3 CMD R 31 25 0.16 0.16 27.5 Y 01 27610 -13.4 -119.3 CMD R 31 25 0.16 0.16 27.5 Y 90 1 27610 -13.4 -119.3 TM T 29.2 22.6 0.16 0.16 30 Y 01 7.3 0.07 17.9

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) CHU R C -99 G16_SCHEDULE_S_CUP.gxt CVU R C -99 G16_SCHEDULE_S_CUP.gxt CHD T C -99 G16_SCHEDULE_S_CDN.gxt -152 -149.5 -149.3 -149.2 -149.1 CVD T C -99 G16_SCHEDULE_S_CDN.gxt -152 -149.5 -149.3 -149.2 -149.1 KHU R C -99 G16_SCHEDULE_S_KUP.gxt KVU R C -99 G16_SCHEDULE_S_KUP.gxt KHD T C -99 G16_SCHEDULE_S_KDN.gxt KVD T C -99 G16_SCHEDULE_S_KDN.gxt UPC T C -99 G16_SCHEDULE_S_KDN.gxt UPC T C -99 G16_SCHEDULE_S_KDN.gxt OMN R C G16_SCHEDULE_S_OMNR.PDF -99 OMN T C G16_SCHEDULE_S_OMNT.PDF -99 -165.9 -165.8 -165.7 -165.6 -165.5 CMD R C -99 G16_SCHEDULE_S_CUP.gxt CMD R C -99 G16_SCHEDULE_S_CUP.gxt TM T C -99 G16_SCHEDULE_S_CDN.gxt -163.3 -163.2 -163.1 -163 -162.9

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) CU1 36 R 5945 V C 1C 127.3 CU1 CVUP CD1 CHDN CU2 36 R 5965 H C 3C 127.3 CU3 CVUP CD3 CHDN CU3 36 R 5985 V C 5C 127.3 CU5 CVUP CD5 CHDN CU4 36 R 6005 H C 7C 127.3 CU7 CVUP CD7 CHDN CU5 36 R 6025 V C 9C 127.3 CU9 CVUP CD9 CHDN CU6 36 R 6045 H C 11C 127.3 CU11 CVUP CD11 CHDN CU7 36 R 6065 V C 13C 127.3 CU13 CVUP CD13 CHDN CU8 36 R 6085 H C 15C 127.3 CU15 CVUP CD15 CHDN CU9 36 R 6105 V C 17C 127.3 CU17 CVUP CD17 CHDN CU10 36 R 6125 H C 19C 127.3 CU19 CVUP CD19 CHDN CU11 36 R 6145 V C 21C 127.3 CU21 CVUP CD21 CHDN CU12 36 R 6165 H C 23C 127.3 CU23 CVUP CD23 CHDN CU13 36 R 6185 V C 2C 127.3 CU2 CHUP CD2 CVDN CU14 36 R 6205 H C 4C 127.3 CU4 CHUP CD4 CVDN CU15 36 R 6225 V C 6C 127.3 CU6 CHUP CD6 CVDN CU16 36 R 6245 H C 8C 127.3 CU8 CHUP CD8 CVDN CU17 36 R 6265 V C 10C 127.3 CU10 CHUP CD10 CVDN CU18 36 R 6285 H C 12C 127.3 CU12 CHUP CD12 CVDN CU19 36 R 6305 V C 14C 127.3 CU14 CHUP CD14 CVDN CU20 36 R 6325 H C 16C 127.3 CU16 CHUP CD16 CVDN CU21 36 R 6345 V C 18C 127.3 CU18 CHUP CD18 CVDN CU22 36 R 6365 H C 20C 127.3 CU20 CHUP CD20 CVDN CU23 36 R 6385 V C 22C 127.3 CU22 CHUP CD22 CVDN CU24 36 R 6405 H C 24C 127.3 CU24 CHUP CD24 CVDN CD1 36 T 3720 H C 1K 134.4 KU1 KVUP KD1 KHDN CD2 36 T 3740 V C 3K 134.4 KU3 KVUP KD3 KHDN CD3 36 T 3760 H C 5K 134.4 KU5 KVUP KD5 KHDN CD4 36 T 3780 V C 7K 134.4 KU7 KVUP KD7 KHDN CD5 36 T 3800 H C 9K 134.4 KU9 KVUP KD9 KHDN CD6 36 T 3820 V C 11K 134.4 KU11 KVUP KD11 KHDN

CD7 36 T 3840 H C 13K 134.4 KU13 KVUP KD13 KHDN CD8 36 T 3860 V C 15K 134.4 KU15 KVUP KD15 KHDN CD9 36 T 3880 H C 17K 134.4 KU17 KVUP KD17 KHDN CD10 36 T 3900 V C 19K 134.4 KU19 KVUP KD19 KHDN CD11 36 T 3920 H C 21K 134.4 KU21 KVUP KD21 KHDN CD12 36 T 3940 V C 23K 134.4 KU23 KVUP KD23 KHDN CD13 36 T 3960 H C 2K 134.4 KU2 KHUP KD2 KVDN CD14 36 T 3980 V C 4K 134.4 KU4 KHUP KD4 KVDN CD15 36 T 4000 H C 6K 134.4 KU6 KHUP KD6 KVDN CD16 36 T 4020 V C 8K 134.4 KU8 KHUP KD8 KVDN CD17 36 T 4040 H C 10K 134.4 KU10 KHUP KD10 KVDN CD18 36 T 4060 V C 12K 134.4 KU12 KHUP KD12 KVDN CD19 36 T 4080 H C 14K 134.4 KU14 KHUP KD14 KVDN CD20 36 T 4100 V C 16K 134.4 KU16 KHUP KD16 KVDN CD21 36 T 4120 H C 18K 134.4 KU18 KHUP KD18 KVDN CD22 36 T 4140 V C 20K 134.4 KU20 KHUP KD20 KVDN CD23 36 T 4160 H C 22K 134.4 KU22 KHUP KD22 KVDN CD24 36 T 4180 V C 24K 134.4 KU24 KHUP KD24 KVDN KU1 36 R 14020 V C TM1 TM1 TM KU2 36 R 14040 H C TM2 TM2 TM KU3 36 R 14060 V C TM3 TM3 OMNT KU4 36 R 14080 H C TM4 TM4 OMNT KU5 36 R 14100 V C UPC1 UPC1 KVDN KU6 36 R 14120 H C UPC2 UPC2 KHDN KU7 36 R 14140 V C CMD1 CMD1 CHUP KU8 36 R 14160 H C CMD2 CMD2 CVUP KU9 36 R 14180 V C CMD3 CMD3 OMNR KU10 36 R 14200 H C CMD4 CMD4 OMNR KU11 36 R 14220 V C KU12 36 R 14240 H C KU13 36 R 14260 V C KU14 36 R 14280 H C KU15 36 R 14300 V C KU16 36 R 14320 H C KU17 36 R 14340 V C KU18 36 R 14360 H C KU19 36 R 14380 V C KU20 36 R 14400 H C KU21 36 R 14420 V C

KU22 36 R 14440 H C KU23 36 R 14460 V C KU24 36 R 14480 H C KD1 36 T 11720 H C KD2 36 T 11740 V C KD3 36 T 11760 H C KD4 36 T 11780 V C KD5 36 T 11800 H C KD6 36 T 11820 V C KD7 36 T 11840 H C KD8 36 T 11860 V C KD9 36 T 11880 H C KD10 36 T 11900 V C KD11 36 T 11920 H C KD12 36 T 11940 V C KD13 36 T 11960 H C KD14 36 T 11980 V C KD15 36 T 12000 H C KD16 36 T 12020 V C KD17 36 T 12040 H C KD18 36 T 12060 V C KD19 36 T 12080 H C KD20 36 T 12100 V C KD21 36 T 12120 H C KD22 36 T 12140 V C KD23 36 T 12160 H C KD24 36 T 12180 V C CMD1 1000 R 5928.75 H T CMD2 1000 R 6424.25 V T CMD3 1000 R 5928.75 L T CMD4 1000 R 6424.25 L T TM1 500 T 4196 H T TM2 500 T 4197 H T TM3 500 T 4196 R T TM4 500 T 4197 R T UPC1 25 T 11701 V C UPC2 25 T 12195 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) D1 30M1G7W 30133 4 36863 0.75 6.1 13.2 D2 6M77G7W 6771 4 6000 0.5 3.9 7.3 D3 77K0G7W 77 4 64 0.5 6.8 12.2 D4 30M1G7W 30133 4 36863 0.75 6.1 12.6 D5 6M77G7W 6771 4 6000 0.5 3.9 11.8 D6 77K0G7W 77 4 64 0.5 6.8 13.9 D7 1M23G7W 1229 2 512 0.5 3.4 10.9 D8 307KG7W 307 2 128 0.5 3.4 9.8

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) A1 36M0F3F 36000 TV/FM 1 NTSC 12.8 2.6 10 13.9 A2 36M0F3F 36000 TV/FM 1 NTSC 12.8 2.6 10 16

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) 1C 24C D1 1 G16_SCHEDU 0 51 17.4 23.4 39.7 43.7 -157.1 20.9 1C 24C D2 3 10300 G16_SCHEDU 0 51 11 17 30.8 34.8 -159.6 19.1 1C 24C D3 287 100 G16_SCHEDU 0 51 -8.2 -2.2 11.6 15.6 -159.3 20.9 1C 24C A1 1 G16_SCHEDU 4 51 17.4 23.4 39.7 43.7 -148.4 26.2 1K 24K D4 1 G16_SCHEDU 0 58.1 17.7 23.7 45.9 51.9 22.3 1K 24K D5 3 10300 G16_SCHEDU 0 58.1 2.2 8.2 36.9 42.9 22.3 1K 24K D6 242 100 G16_SCHEDU 0 58.1 -16.1 -10.1 20.6 24.6 22.3 1K 24K D7 24 1450 G16_SCHEDU 0 58.1 -7.1 -3.1 29.6 33.6 22.3 1K 24K D8 90 400 G16_SCHEDU 0 46.4 -4.5 -0.5 20.5 24.5 34.6 1K 24K A2 1 G16_SCHEDU 4 58.1 17.7 23.7 45.9 51.9 26.7

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): No

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 1859.3 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2545.8 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4405.1 24.8 0.91 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 716 6.4 0.866 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 74.5 6.4 0.788 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): 7241 7241 7241 7241 Bus (Watts): (b): (g): (l): (q): 1900 966 1900 966 Total (Watts): (c): (h): (m): (r): 9141 8207 9141 8207 Solar Array (Watts): (d): (i): (n): (s): 10148 9218 9871 8965 Depth of Battery (e) (j) (o) (t) Discharge (%): 75 % % 77.6 % % 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: 2006-03-07 16:20:03
Document Modified: 2006-03-07 16:20:03
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