Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20080825-00159 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2008082500159_661214

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 25 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: 52 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: 93.1 W PROVIDE ADDITIONAL AND BACK-UP CAPACITY Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be TO GALAXY 26 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 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 30.4 26.4 1 2.6 -95.3 21 1 CVU R 30.4 26.4 1 2.6 -95.3 21 1 KHU R 30.1 26.1 1 2.7 -98 21 1 KVU R 30.1 26.1 1 2.7 -98 21 1 CHD T 28.3 24.3 1 39.3 CVD T 28.3 24.3 1 39.3 KHD T 31.4 27.4 1 47.7 KVD T 31.4 27.4 1 47.7 CMW R 2 -4.5 2 -34.1 -97.9 CMW R 2 -4.5 2 -34.1 -97.9 CMM R 4 -2.5 2 -31.2 -100.8 CMM R 4 -2.5 2 -31.2 -100.8 TMO T 29 19 1 24.5 TMW T 2 -4.5 2 8.8 TMM T 2 -4.5 2 5.2 BCN T 31.3 27.3 1 26 BCN T 31.3 27.3 1 26

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 -93.1 chup.gxt CVU R C -93.1 cvup.gxt KHU R C -93.1 khup.gxt KVU R C -93.1 kvup.gxt CHD T C -93.1 chdn.gxt -154 -153.9 -153.7 -153.6 -153.5 CVD T C -93.1 cvdn.gxt -154 -153.9 -153.7 -153.6 -153.5 KHD T C -93.1 khdn.gxt KVD T C -93.1 kvdn.gxt CMW R C -93.1 cmwh.pdf CMW R C -93.1 cmwv.pdf CMM R C -93.1 cmmh.pdf CMM R C -93.1 cmmv.pdf TMO T C -93.1 tmov.gxt -156.7 -156.6 -156.5 -156.4 -156.3 TMW T C -93.1 tmwv.pdf -172.4 -172.3 -172.2 -172.1 -172 TMM T C -93.1 tmmv.pdf -176 -175.9 -175.8 -175.7 -175.6 BCN T C -93.1 bcnh.gxt BCN T C -93.1 bcnv.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) CU001 36000 R 5945 H C C0001 114.9 CU001 CHUP CD001 CVDN CU002 36000 R 5965 V C C0003 114.9 CU003 CHUP CD003 CVDN CU003 36000 R 5985 H C C0005 114.9 CU005 CHUP CD005 CVDN CU004 36000 R 6005 V C C0007 114.9 CU007 CHUP CD007 CVDN CU005 36000 R 6025 H C C0009 114.9 CU009 CHUP CD009 CVDN CU006 36000 R 6045 V C C0011 114.9 CU011 CHUP CD011 CVDN CU007 36000 R 6065 H C C0013 114.9 CU013 CHUP CD013 CVDN CU008 36000 R 6085 V C C0015 114.9 CU015 CHUP CD015 CVDN CU009 36000 R 6105 H C C0017 114.9 CU017 CHUP CD017 CVDN CU010 36000 R 6125 V C C0019 114.9 CU019 CHUP CD019 CVDN CU011 36000 R 6145 H C C0021 114.9 CU021 CHUP CD021 CVDN CU012 36000 R 6165 V C C0023 114.9 CU023 CHUP CD023 CVDN CU013 36000 R 6185 H C C0002 114.9 CU002 CVUP CD002 CHDN CU014 36000 R 6205 V C C0004 114.9 CU004 CVUP CD004 CHDN CU015 36000 R 6225 H C C0006 114.9 CU006 CVUP CD006 CHDN CU016 36000 R 6245 V C C0008 114.9 CU008 CVUP CD008 CHDN CU017 36000 R 6265 H C C0010 114.9 CU010 CVUP CD010 CHDN CU018 36000 R 6285 V C C0012 114.9 CU012 CVUP CD012 CHDN CU019 36000 R 6305 H C C0014 114.9 CU014 CVUP CD014 CHDN CU020 36000 R 6325 V C C0016 114.9 CU016 CVUP CD016 CHDN CU021 36000 R 6345 H C C0018 114.9 CU018 CVUP CD018 CHDN CU022 36000 R 6365 V C C0020 114.9 CU020 CVUP CD020 CHDN CU023 36000 R 6385 H C C0022 114.9 CU022 CVUP CD022 CHDN CU024 36000 R 6405 V C C0024 114.9 CU024 CVUP CD024 CHDN CD001 36000 T 3720 V C K0001 127.8 KU001 KHUP KD001 KVDN CD002 36000 T 3740 H C K0003 127.8 KU003 KHUP KD003 KVDN CD003 36000 T 3760 V C K0005 127.8 KU005 KHUP KD005 KVDN CD004 36000 T 3780 H C K0007 127.8 KU007 KHUP KD007 KVDN CD005 36000 T 3800 V C K0009 127.8 KU009 KHUP KD009 KVDN CD006 36000 T 3820 H C K0011 127.8 KU011 KHUP KD011 KVDN

CD007 36000 T 3840 V C K0013 127.8 KU013 KHUP KD013 KVDN CD008 36000 T 3860 H C K0015 127.8 KU015 KHUP KD015 KVDN CD009 36000 T 3880 V C K0017 127.8 KU017 KHUP KD017 KVDN CD010 36000 T 3900 H C K0019 127.8 KU019 KHUP KD019 KVDN CD011 36000 T 3920 V C K0021 127.8 KU021 KHUP KD021 KVDN CD012 36000 T 3940 H C K0023 127.8 KU023 KHUP KD023 KVDN CD013 36000 T 3960 V C K0025 127.8 KU025 KHUP KD025 KVDN CD014 36000 T 3980 H C K0027 127.8 KU027 KHUP KD027 KVDN CD015 36000 T 4000 V C K0002 127.8 KU002 KVUP KD002 KHDN CD016 36000 T 4020 H C K0004 127.8 KU004 KVUP KD004 KHDN CD017 36000 T 4040 V C K0006 127.8 KU006 KVUP KD006 KHDN CD018 36000 T 4060 H C K0008 127.8 KU008 KVUP KD008 KHDN CD019 36000 T 4080 V C K0010 127.8 KU010 KVUP KD010 KHDN CD020 36000 T 4100 H C K0012 127.8 KU012 KVUP KD012 KHDN CD021 36000 T 4120 V C K0014 127.8 KU014 KVUP KD014 KHDN CD022 36000 T 4140 H C K0016 127.8 KU016 KVUP KD016 KHDN CD023 36000 T 4160 V C K0018 127.8 KU018 KVUP KD018 KHDN CD024 36000 T 4180 H C K0020 127.8 KU020 KVUP KD020 KHDN KU001 54000 R 14028.5 H C K0022 127.8 KU022 KVUP KD022 KHDN KU002 54000 R 14035.0 V C K0024 127.8 KU024 KVUP KD024 KHDN KU003 54000 R 14089.5 H C K0026 127.8 KU026 KVUP KD026 KHDN KU004 54000 R 14096.0 V C K0028 127.8 KU028 KVUP KD028 KHDN KU005 27000 R 14136 H C KU007 27000 R 14167 H C KU009 27000 R 14198 H C KU011 27000 R 14229 H C KU013 27000 R 14260 H C KU015 27000 R 14291 H C KU017 27000 R 14322 H C KU019 27000 R 14353 H C KU021 27000 R 14384 H C KU023 27000 R 14415 H C KU025 27000 R 14446 H C KU027 27000 R 14477 H C KU006 27000 R 14142.5 V C KU008 27000 R 14173.5 V C KU010 27000 R 14204.5 V C KU012 27000 R 14235.5 V C KU014 27000 R 14266.5 V C

KU016 27000 R 14297.5 V C KU018 27000 R 14328.5 V C KU020 27000 R 14359.5 V C KU022 27000 R 14390.5 V C KU024 27000 R 14421.5 V C KU026 27000 R 14452.5 V C KU028 27000 R 14483.5 V C KD001 54000 T 11728.5 V C KD002 54000 T 11735 H C KD003 54000 T 11789.5 V C KD004 54000 T 11796 H C KD005 27000 T 11836 V C KD007 27000 T 11867 V C KD009 27000 T 11898 V C KD011 27000 T 11929 V C KD013 27000 T 11960 V C KD015 27000 T 11991 V C KD017 27000 T 12022 V C KD019 27000 T 12053 V C KD021 27000 T 12084 V C KD023 27000 T 12115 V C KD025 27000 T 12146 V C KD027 27000 T 12177 V C KD006 27000 T 11842.5 H C KD008 27000 T 11873.5 H C KD010 27000 T 11904.5 H C KD012 27000 T 11935.5 H C KD014 27000 T 11966.5 H C KD016 27000 T 11997.5 H C KD018 27000 T 12028.5 H C KD020 27000 T 12059.5 H C KD022 27000 T 12090.5 H C KD024 27000 T 12121.5 H C KD026 27000 T 12152.5 H C KD028 27000 T 12183.5 H C CMD1 1000 R 5926.5 V T CMD2 1000 R 6423.5 H T CMD3 1000 R 5926.5 V T CMD4 1000 R 6423.5 H T

TLM1 500 T 4195.5 V T TLM2 500 T 4199.5 V T TLM3 500 T 4195.5 V T TLM4 500 T 4199.5 V T TLM5 500 T 4195.5 V T TLM6 500 T 4199.5 V T UPC1 25 T 11702 H T UPC2 25 T 12198 V 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 54M0G7W 54000 4 45801 0.667 5.1 17.8 D2 36M0G7W 36000 4 36863 0.75 6.1 13.6 D3 27M0G7W 27000 4 24575 0.667 5.1 18.6 D4 10M3G7W 10300 4 6000 0.5 3.9 16.7 D5 100KG7W 100 4 64 0.5 3 15.8 D6 1M45G7W 1450 2 512 0.5 3.4 15.7 D7 400KG7W 400 2 128 0.5 3.4 17.6

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 16.1 A2 24M0F3F 24000 TV/FM 1 NTSC 12.8 2.6 10 23

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) C0001 C0024 A1 1 LINK BUDGET 4000 51 20.6 24.6 35.3 39.3 -152.8 26.2 C0001 C0024 D2 1 LINK BUDGET 49.4 19.2 23.2 35.3 39.3 -161.5 21 C0001 C0024 D4 2 LINK BUDGET 49.4 10.5 14.5 28 32 -162.4 19.2 C0001 C0024 D5 257 LINK BUDGET 49.4 -9.9 -5.9 7.6 11.6 -163.3 19.2 K0005 K0028 A2 1 LINK BUDGET 4000 56.9 18 22 38.2 42.2 -149.9 31 K0005 K0028 D3 1 LINK BUDGET 56.9 19.5 23.5 39.5 43.5 -156.1 25 K0005 K0028 D4 2 LINK BUDGET 56.9 3.9 7.9 33 37 -157.4 25 K0005 K0028 D5 267 LINK BUDGET 56.9 -14.3 -10.3 14.8 18.8 -156.1 22.3 K0005 K0028 D6 16 LINK BUDGET 56.9 -2.3 1.7 26.8 30.8 -156.2 22.3 K0005 K0028 D7 67 LINK BUDGET 46.4 -3.1 0.9 15.4 19.4 -161.6 33.1 K0001 K0004 A2 2 LINK BUDGET 4000 56.9 18 22 36.9 40.9 -151.2 33.1 K0001 K0004 D1 1 LINK BUDGET 58.1 21 25 41.4 45.4 -156.9 25 K0001 K0004 D4 3 LINK BUDGET 56.9 1.1 5.1 33.2 37.2 -157.2 25 K0001 K0004 D5 403 LINK BUDGET 56.9 -19.1 -15.1 13 17 -157.9 25 K0001 K0004 D6 25 LINK BUDGET 56.9 -7.1 -3.1 25 29 -158 25 K0001 K0004 D7 135 LINK BUDGET 49 -8.4 -4.4 15.8 19.8 -161.2 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, 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: S16. SPACECRAFT ELECTRICAL CHARACTERISTICS: S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: 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 # 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? 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: 2008-08-27 17:06:34
Document Modified: 2008-08-27 17:06:34
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