Attachment Schedule S Tech Data

This document pretains to SAT-RPL-20070222-00035 for Replacement Application on a Satellite Space Stations filing.

IBFS_SATRPL2007022200035_551668

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 18 6/30/2008 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 1/1/2006 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 3/11/2007 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: 10/1/2007 3/31/2008 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: 123 W REPLACEMENT FOR GALAXY 10R 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 UNITED STATES, ALASKA, HAWAII, PUERTO RICO AND PORTIONS OF CANADA AND ME 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 31.8 25.8 0.17 0.16 29 Y 01 434 5.4 -107.2 31 1 CVU R 31.8 25.8 0.17 0.16 29 Y 90 1 434 5.4 -107.2 31 1 CHD T 30.1 26.1 0.17 0.16 30 Y 0 1 1.4 43.7 46.5 CVD T 30.1 26.1 0.17 0.16 30 Y 90 1 1.4 43.7 46.5 KHU R 35.6 25.6 0.17 0.16 27 N 0 1 540 8.3 -107.9 31 1 KVUL R 35.6 25.6 0.17 0.16 27 N 90 1 540 8.3 -107.9 31 1 KHD T 34.9 26.9 0.17 0.16 26 N 0 1 2 74.1 53.6 KVDL T 34.9 26.9 0.17 0.16 26 N 90 1 2 74.1 53.6 CMD R 31.8 25.8 0.17 0.16 Y 0 1 27610 -12.6 -114.5 CMD R 31.8 25.8 0.17 0.16 Y 90 1 27610 -12.6 -114.5 CMD R 5.4 -0.6 0.17 0.16 Y 2 9235 -34.3 -97.8 TLM T 30.1 25.1 0.17 0.16 Y 90 1 7.3 0.07 18.8 TLM T 5.6 -4.4 0.17 0.16 Y 2 6.8 9.3 15.3 UPC T 34.9 24.9 0.17 0.16 N 01 10 0.02 18.4 UPC T 34.9 24.9 0.17 0.16 N 90 1 10 0.02 18.4

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 -123 CHUL.gxt CVU R C -123 CVUL.gxt CHD T C -123 CHDL.gxt -152 -149.5 -147 -146.4 -146.3 CVD T C -123 CVDL.gxt -152 -149.5 -147 -146.4 -146.3 KHU R C -123 KHUL.gxt KVUL R C -123 KVUL.gxt KHD T C -123 KHDL.gxt KVDL T C -123 KVDL.gxt CMD R C -123 CDMH.gxt CMD R C -123 CDMV.gxt CMD R C -123 CMDW.pdf TLM T C -123 TLMV.gxt -162.4 -162.3 -162.2 -162.1 -162 TLM T C -123 TLMW.pdf -165.9 -165.8 -165.7 -165.6 -165.5 UPC T C -123 UPCH.gxt UPC T C -123 UPCV.gxt CHU R X -123 CHUX.gxt CVU R X -123 CVUX.gxt CHD T X -123 CHDX.gxt CVD T X -123 CVDX.gxt KHU R X -123 KHUX.gxt KVUL R X -123 KVUX.gxt KHD T X -123 KHDX.gxt KVDL T X -123 KVDX.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) CU1 36000 R 5945 H C 1C 129.1 CU1 CHUL CD1 CVDL CU3 36000 R 5985 H C 3C 129.1 CU3 CHUL CD3 CVDL CU5 36000 R 6025 H C 5C 129.1 CU5 CHUL CD5 CVDL CU7 36000 R 6065 H C 7C 129.1 CU7 CHUL CD7 CVDL CU9 36000 R 6105 H C 9C 129.1 CU9 CHUL CD9 CVDL CU11 36000 R 6145 H C 11C 129.1 CU11 CHUL CD11 CVDL CU13 36000 R 6185 H C 13C 129.1 CU13 CHUL CD13 CVDL CU15 36000 R 6225 H C 15C 129.1 CU15 CHUL CD15 CVDL CU17 36000 R 6265 H C 17C 129.1 CU17 CHUL CD17 CVDL CU19 36000 R 6305 H C 19C 129.1 CU19 CHUL CD19 CVDL CU21 36000 R 6345 H C 21C 129.1 CU21 CHUL CD21 CVDL CU23 36000 R 6385 H C 23C 129.1 CU23 CHUL CD23 CVDL CU2 36000 R 5965 V C 2C 129.1 CU2 CVUL CD2 CHDL CU4 36000 R 6005 V C 4C 129.1 CU4 CVUL CD4 CHDL CU6 36000 R 6045 V C 6C 129.1 CU6 CVUL CD6 CHDL CU8 36000 R 6085 V C 8C 129.1 CU8 CVUL CD8 CHDL CU10 36000 R 6125 V C 10C 129.1 CU10 CVUL CD10 CHDL CU12 36000 R 6165 V C 12C 129.1 CU12 CVUL CD12 CHDL CU14 36000 R 6205 V C 14C 129.1 CU14 CVUL CD14 CHDL CU16 36000 R 6245 V C 16C 129.1 CU16 CVUL CD16 CHDL CU18 36000 R 6285 V C 18C 129.1 CU18 CVUL CD18 CHDL CU20 36000 R 6325 V C 20C 129.1 CU20 CVUL CD20 CHDL CU22 36000 R 6365 V C 22C 129.1 CU22 CVUL CD22 CHDL CU24 36000 R 6405 V C 24C 129.1 CU24 CVUL CD24 CHDL CD1 36000 T 3720 V C 1K 135.6 KU1 KHUL KD1 KVDL CD3 36000 T 3760 V C 3K 135.6 KU3 KHUL KD3 KVDL CD5 36000 T 3800 V C 5K 135.6 KU5 KHUL KD5 KVDL CD7 36000 T 3840 V C 7K 135.6 KU7 KHUL KD7 KVDL CD9 36000 T 3880 V C 9K 135.6 KU9 KHUL KD9 KVDL CD11 36000 T 3920 V C 11K 135.6 KU11 KHUL KD11 KVDL

CD13 36000 T 3960 V C 13K 135.6 KU13 KHUL KD13 KVDL CD15 36000 T 4000 V C 15K 135.6 KU15 KHUL KD15 KVDL CD17 36000 T 4040 V C 17K 135.6 KU17 KHUL KD17 KVDL CD19 36000 T 4080 V C 19K 135.6 KU19 KHUL KD19 KVDL CD21 36000 T 4120 V C 21K 135.6 KU21 KHUL KD21 KVDL CD23 36000 T 4160 V C 23K 135.6 KU23 KHUL KD23 KVDL CD2 36000 T 3740 H C 2K 135.6 KU2 KVUL KD2 KHDL CD4 36000 T 3780 H C 4K 135.6 KU4 KVUL KD4 KHDL CD6 36000 T 3820 H C 6K 135.6 KU6 KVUL KD6 KHDL CD8 36000 T 3860 H C 8K 135.6 KU8 KVUL KD8 KHDL CD10 36000 T 3900 H C 10K 135.6 KU10 KVUL KD10 KHDL CD12 36000 T 3940 H C 12K 135.6 KU12 KVUL KD12 KHDL CD14 36000 T 3980 H C 14K 135.6 KU14 KVUL KD14 KHDL CD16 36000 T 4020 H C 16K 135.6 KU16 KVUL KD16 KHDL CD18 36000 T 4060 H C 18K 135.6 KU18 KVUL KD18 KHDL CD20 36000 T 4100 H C 20K 135.6 KU20 KVUL KD20 KHDL CD22 36000 T 4140 H C 22K 135.6 KU22 KVUL KD22 KHDL CD24 36000 T 4180 H C 24K 135.6 KU24 KVUL KD24 KHDL KU1 36000 R 14020 H C KU3 36000 R 14060 H C KU5 36000 R 14100 H C KU7 36000 R 14140 H C KU9 36000 R 14180 H C KU11 36000 R 14220 H C KU13 36000 R 14260 H C KU15 36000 R 14300 H C KU17 36000 R 14340 H C KU19 36000 R 14380 H C KU21 36000 R 14420 H C KU23 36000 R 14460 H C KU2 36000 R 14040 V C KU4 36000 R 14080 V C KU6 36000 R 14120 V C KU8 36000 R 14160 V C KU10 36000 R 14200 V C KU12 36000 R 14240 V C KU14 36000 R 14280 V C KU16 36000 R 14320 V C KU18 36000 R 14360 V C

KU20 36000 R 14400 V C KU22 36000 R 14440 V C KU24 36000 R 14480 V C KD1 36000 T 11720 V C KD3 36000 T 11760 V C KD5 36000 T 11800 V C KD7 36000 T 11840 V C KD9 36000 T 11880 V C KD11 36000 T 11920 V C KD13 36000 T 11960 V C KD15 36000 T 12000 V C KD17 36000 T 12040 V C KD19 36000 T 12080 V C KD21 36000 T 12120 V C KD23 36000 T 12160 V C KD2 36000 T 11740 H C KD4 36000 T 11780 H C KD6 36000 T 11820 H C KD8 36000 T 11860 H C KD10 36000 T 11900 H C KD12 36000 T 11940 H C KD14 36000 T 11980 H C KD16 36000 T 12020 H C KD18 36000 T 12060 H C KD20 36000 T 12100 H C KD22 36000 T 12140 H C KD24 36000 T 12180 H C CMD1 1000 R 5926.5 V T CMD2 1000 R 6424.5 H T CMD3 1000 R 5926.5 L T CMD4 1000 R 6424.5 L T TLM1 500 T 4197.125 V T TLM2 500 T 4198.875 V T TLM3 500 T 4197.125 R T TLM4 500 T 4198.875 R T UPC1 25 T 11701 H C UPC2 25 T 12195 V 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 16.5 D2 4M15G7W 4154 4 6000 0.75 6.7 15.9 D3 1M21G7W 1212.8 4 1544 0.75 5.7 14.7 D4 75K4G7W 75.4 4 64 0.5 3 16.3 D5 6M77G7W 6771.1 4 6000 0.5 3.9 18.3 D6 1M82G7W 1819.2 4 1544 0.5 3 16.2 D7 1M23G7W 1229 2 512 0.5 3.4 15.1 D8 307KG7W 307 2 128 0.5 3.4 16.4

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 21.2

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 A1 1 G18_SCHEDU 4000 49.4 17.3 23.3 42.5 46.5 -145.6 23.6 1C 24C D1 1 G18_SCHEDU 49.4 17.3 23.3 42.5 46.5 -154.3 19.2 1C 24C D2 3 6875 G18_SCHEDU 49.4 7.7 13.7 33.4 37.4 -154.9 19.2 1C 24C D3 16 1550 G18_SCHEDU 49.4 1.2 7.2 26.9 30.9 -156 19.2 1C 24C D4 360 100 G18_SCHEDU 49.4 -13.5 -7.5 12.2 16.2 -158.7 19.2 1K 24K A1 1 G18_SCHEDU 4000 60.2 11.3 21.3 35 43 -149.1 41.9 1K 24K D1 1 G18_SCHEDU 58.1 13.2 23.2 36.8 44.8 -156.1 31 1K 24K D5 3 10300 G18_SCHEDU 58.1 8.1 18.1 30.3 38.3 -156.1 33.1 1K 24K D6 15 2325 G18_SCHEDU 58.1 2.1 12.1 24.3 32.3 -156.4 31 1K 24K D4 360 100 G18_SCHEDU 58.1 -11.6 -1.6 10.6 18.6 -156.3 31 1K 24K D7 24 1450 G18_SCHEDU 58.1 -6.3 3.7 22.9 30.9 -156.1 31 1K 24K D8 90 400 G18_SCHEDU 54.7 -9.7 0.3 16.1 24.1 -156.9 34.6

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: 3400 INTERNATIONAL DRIVE, N.W. S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: WASHINGTON, D.C. DC 20008 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 202-944-7701

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 1911 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2825 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4736 24.8 0.89 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 864 6.4 0.877 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 74.5 6.4 0.781 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): 7376 7376 7376 7376 Bus (Watts): (b): (g): (l): (q): 1906 973 967 775 Total (Watts): (c): (h): (m): (r): 9282 8349 8343 8151 Solar Array (Watts): (d): (i): (n): (s): 11977 10747 10571 9676 Depth of Battery (e) (j) (o) (t) Discharge (%): 73.2 % % 76.3 % % 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: 2007-02-26 12:38:27
Document Modified: 2007-02-26 12:38:27
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