Attachment Schedule S Tech Data

This document pretains to SAT-AMD-20070123-00013 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2007012300013_546590

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 17 7/30/2007 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 8/30/2005 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 3/8/2007 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: 4/15/2007 6/23/2007 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: 91 W Replaces Galaxy 11 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, Hawaii, Portions of Canada and Mexico 2 S Continental United States, Hawaii, Puerto Rico, Portion of Canada 3 S Visible Earth

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) CUP R 31.7 26.7 0.12 0.28 27 Y 1 447 5.2 -114.2 47 1 CDN T 28.6 25.6 0.12 0.28 25 Y 1 2 29.5 43.3 KUP R 33.7 27.7 0.12 0.28 30 Y 2 453 7.1 -119.1 47 1 KDN T 33.1 29.1 0.12 0.28 29 Y 2 2.3 66.1 51.3 UPC T 33.1 29.1 0.12 0.28 29 Y 2 3.7 0.17 25.4 CMD R 31.7 21.7 0.12 0.28 27 Y 1 11396 -8.9 -122.5 TLM T 28.6 18.6 0.12 0.28 25 Y 1 6.8 0.08 17.8 OCM R 8 6 0.12 0.28 N 3 2431 -25.9 -105.3 OTL T 7.8 5.8 0.12 0.28 N 3 7.3 8.7 17.2

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) CUP R C -91 CUP.gxt CDN T C -91 CDN.gxt -152 -149.9 -149.7 -149.6 -149.5 KUP R C -91 KUP.gxt KDN T C -91 KDN.gxt UPC T C -91 UPC.gxt CMD R C -91 CMD.gxt TLM T C -91 TLM.gxt -158 -157.9 -157.8 -157.7 -157.6 OCM R C -91 OCMD.PDF OTL T C -91 OTLM.PDF -158.6 -158.5 -158.4 -158.3 -158.2 CUP R X -91 CUPX.gxt CDN T X -91 CDNX.gxt KUP R X -91 KUPX.gxt KDN T X -91 KDNX.gxt UPC T X -91 UPCX.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) UC1 36000 R 5945 V C 1C 134.5 UC1 CUP DC1 CDN UC3 36000 R 5985 V C 2C 134.5 UC2 CUP DC2 CDN UC5 36000 R 6025 V C 3C 134.5 UC3 CUP DC3 CDN UC7 36000 R 6065 V C 4C 134.5 UC4 CUP DC4 CDN UC9 36000 R 6105 V C 5C 134.5 UC5 CUP DC5 CDN UC11 36000 R 6145 V C 6C 134.5 UC6 CUP DC6 CDN UC13 36000 R 6185 V C 7C 134.5 UC7 CUP DC7 CDN UC15 36000 R 6225 V C 8C 134.5 UC8 CUP DC8 CDN UC17 36000 R 6265 V C 9C 134.5 UC9 CUP DC9 CDN UC19 36000 R 6305 V C 10C 134.5 UC10 CUP DC10 CDN UC21 36000 R 6345 V C 11C 134.5 UC11 CUP DC11 CDN UC23 36000 R 6385 V C 12C 134.5 UC12 CUP DC12 CDN UC2 36000 R 5965 H C 13C 134.5 UC13 CUP DC13 CDN UC4 36000 R 6005 H C 14C 134.5 UC14 CUP DC14 CDN UC6 36000 R 6045 H C 15C 134.5 UC15 CUP DC15 CDN UC8 36000 R 6085 H C 16C 134.5 UC16 CUP DC16 CDN UC10 36000 R 6125 H C 17C 134.5 UC17 CUP DC17 CDN UC12 36000 R 6165 H C 18C 134.5 UC18 CUP DC18 CDN UC14 36000 R 6205 H C 19C 134.5 UC19 CUP DC19 CDN UC16 36000 R 6245 H C 20C 134.5 UC20 CUP DC20 CDN UC18 36000 R 6285 H C 21C 134.5 UC21 CUP DC21 CDN UC20 36000 R 6325 H C 22C 134.5 UC22 CUP DC22 CDN UC22 36000 R 6365 H C 23C 134.5 UC23 CUP DC23 CDN UC24 36000 R 6405 H C 24C 134.5 UC24 CUP DC24 CDN DC1 36000 T 3720 H C 1K 148.1 UK1 KUP DK1 KDN DC3 36000 T 3760 H C 2K 148.1 UK2 KUP DK2 KDN DC5 36000 T 3800 H C 3K 148.1 UK3 KUP DK3 KDN DC7 36000 T 3840 H C 4K 148.1 UK4 KUP DK4 KDN DC9 36000 T 3880 H C 5K 148.1 UK5 KUP DK5 KDN DC11 36000 T 3920 H C 6K 148.1 UK6 KUP DK6 KDN

DC13 36000 T 3960 H C 7K 148.1 UK7 KUP DK7 KDN DC15 36000 T 4000 H C 8K 148.1 UK8 KUP DK8 KDN DC17 36000 T 4040 H C 9K 148.1 UK9 KUP DK9 KDN DC19 36000 T 4080 H C 10K 148.1 UK10 KUP DK10 KDN DC21 36000 T 4120 H C 11K 148.1 UK11 KUP DK11 KDN DC23 36000 T 4160 H C 12K 148.1 UK12 KUP DK12 KDN DC2 36000 T 3740 V C 13K 148.1 UK13 KUP DK13 KDN DC4 36000 T 3780 V C 14K 148.1 UK14 KUP DK14 KDN DC6 36000 T 3820 V C 15K 148.1 UK15 KUP DK15 KDN DC8 36000 T 3860 V C 16K 148.1 UK16 KUP DK16 KDN DC10 36000 T 3900 V C 17K 148.1 UK17 KUP DK17 KDN DC12 36000 T 3940 V C 18K 148.1 UK18 KUP DK18 KDN DC14 36000 T 3980 V C 19K 148.1 UK19 KUP DK19 KDN DC16 36000 T 4020 V C 20K 148.1 UK20 KUP DK20 KDN DC18 36000 T 4060 V C 21K 148.1 UK21 KUP DK21 KDN DC20 36000 T 4100 V C 22K 148.1 UK22 KUP DK22 KDN DC22 36000 T 4140 V C 23K 148.1 UK23 KUP DK23 KDN DC24 36000 T 4180 V C 24K 148.1 UK24 KUP DK24 KDN CMD1 1000 R 5925.5 H T CMD2 1000 R 6424.5 V T CMD3 1000 R 5925.5 L T CMD4 1000 R 6424.5 R T TLM1 500 T 4197.125 H T TLM2 500 T 4198.875 H T TLM3 500 T 4197.125 L T TLM4 500 T 4198.875 R T UPC1 25 T 11701 V C UPC2 25 T 12195 H C UK1 36000 R 14020 V C UK3 36000 R 14060 V C UK5 36000 R 14100 V C UK7 36000 R 14140 V C UK9 36000 R 14180 V C UK11 36000 R 14220 V C UK13 36000 R 14260 V C UK15 36000 R 14300 V C UK17 36000 R 14340 V C UK19 36000 R 14380 V C UK21 36000 R 14420 V C

UK23 36000 R 14460 V C UK2 36000 R 14040 H C UK4 36000 R 14080 H C UK6 36000 R 14120 H C UK8 36000 R 14160 H C UK10 36000 R 14200 H C UK12 36000 R 14240 H C UK14 36000 R 14280 H C UK16 36000 R 14320 H C UK18 36000 R 14360 H C UK20 36000 R 14400 H C UK22 36000 R 14440 H C UK24 36000 R 14480 H C DK1 36000 T 11720 H C DK3 36000 T 11760 H C DK5 36000 T 11800 H C DK7 36000 T 11840 H C DK9 36000 T 11880 H C DK11 36000 T 11920 H C DK13 36000 T 11960 H C DK15 36000 T 12000 H C DK17 36000 T 12040 H C DK19 36000 T 12080 H C DK21 36000 T 12120 H C DK23 36000 T 12160 H C DK2 36000 T 11740 V C DK4 36000 T 11780 V C DK6 36000 T 11820 V C DK8 36000 T 11860 V C DK10 36000 T 11900 V C DK12 36000 T 11940 V C DK14 36000 T 11980 V C DK16 36000 T 12020 V C DK18 36000 T 12060 V C DK20 36000 T 12100 V C DK22 36000 T 12140 V C DK24 36000 T 12180 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 16.3 D2 4M15G7W 4154 4 6000 0.75 6.7 16.4 D3 1M21G7W 1212.8 4 1544 0.75 5.7 15.6 D4 75K4G7W 75.4 4 64 0.75 3 13.4 D5 1M23G7W 1229 2 512 0.5 3.4 13.3 D6 307KG7W 307 2 128 0.5 3.4 12.9

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) A1 36M0F3F 36000 TV/FM 1 NTSC 12.8 2.6 10 20.2

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 G17 SCHEDUL 4 52.8 18.9 23.9 40.3 43.3 -148.8 23.6 1C 24C D1 1 NOTE.txt 52.8 18.9 23.9 40.3 43.3 -157.5 19.2 1C 24C D2 5 6875 NOTE.txt 52.8 6.3 11.3 29.2 32.2 -160.1 21 1C 24C D3 23 1550 NOTE.txt 52.8 -0.2 4.8 22.7 25.7 -161.2 21 1C 24C D4 360 100 NOTE.txt 52.8 -11.9 -6.9 11 14 -160.9 19.2 1K 24K A1 1 NOTE.txt 4 56.9 16.9 22.9 47.3 51.3 -140.8 25 1K 24K D1 1 NOTE.txt 56.9 16.9 22.9 47.3 51.3 -149.6 18.8 1K 24K D2 5 6875 NOTE.txt 56.9 3.9 9.9 36.8 40.8 -151.5 22.3 1K 24K D3 20 1550 NOTE.txt 56.9 -2.3 3.7 30.6 34.6 -152.3 22.3 1K 24K D4 322 100 NOTE.txt 56.9 -14.2 -8.2 18.7 22.7 -152.2 18.8 1K 24K D5 20 1450 NOTE.txt 56.9 -2.2 3.8 30.7 34.7 -152.3 18.8 1K 24K D6 90 400 NOTE.txt 42.9 -1.4 4.6 17.5 21.5 -159.5 33.1

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, NW S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Washington, DC 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 1777 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2323 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4100 5.3 0.938 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 707 3.3 0.802 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 66 2.3 0.752 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): 6187 6187 6187 6187 Bus (Watts): (b): (g): (l): (q): 1713 921 1713 921 Total (Watts): (c): (h): (m): (r): 7900 7108 7900 7108 Solar Array (Watts): (d): (i): (n): (s): 10738 9603 8891 8043 Depth of Battery (e) (j) (o) (t) Discharge (%): 64 % % 61 % % 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: 2007-01-24 10:54:13
Document Modified: 2007-01-24 10:54:13
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