Attachment Sched S Tech Report

This document pretains to SAT-MOD-20101029-00228 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2010102900228_850505

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: NEW DAWN 6/30/2011 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 9/30/2008 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 1/14/2011 30 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: 2/18/2011 3/31/2011 1872 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) 5850 M 6500 M R Fixed Satellite Service 14000 M 14500 M R Fixed Satellite Service 3625 M 4200 M T Fixed Satellite Service 10950 M 11200 M T Fixed Satellite Service 11450 M 11700 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: 32.8 E REPLACE THE EXISTING GALAXY 11 SPACECRAFT 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 AFRICA, EUROPE, MIDDLE EAST 2 S SOUTHWESTERN AFRICA 3 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) LLUP R 27.1 19.1 0.12 0.12 30 N 1 550 -0.3 -111 31 1 LRU R 27.1 19.1 0.12 0.12 30 N 1 562 -0.4 -111 31 1 AHU R 33.8 23.8 0.12 0.12 30 N 02 708 5.3 -114.4 32 1 AVU R 33.8 23.8 0.12 0.12 30 N 90 2 708 5.3 -114.4 32 1 LRD T 27.7 19.7 0.12 0.12 30 N 1 2.5 28.2 42.2 LLDN T 27.7 19.7 0.12 0.12 30 N 1 2.5 28.2 42.2 AHD T 31.9 23.9 0.12 0.12 30 N 02 3 75.9 50.7 AVD T 32.2 24.2 0.12 0.12 30 N 90 2 2.9 77.6 51.1 CMD R 20.8 16.8 0.12 0.12 N 3 7756 -18.1 -116.2 CMD R 13.6 9.6 0.12 0.12 N 3 12089 -27.2 -107.1 CMD R 2.5 -1.5 0.12 0.12 N 3 8719 -36.9 -97.4 TLM T 20.2 16.2 0.12 0.12 N 3 5.3 0.2 12.5 TLM T 13.3 9.3 0.12 0.12 N 3 8.3 1.5 15 TLM T 2.3 -1.7 0.12 0.12 N 3 5.2 3 7.1 UPC T 13 9 0.12 0.12 N 90 3 1.6 0.7 11.4 UPC T 20.6 16.6 0.12 0.12 N 3 2.9 0.2 13.9

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) LLUP R C 32.8 LLUP.gxt LRU R C 32.8 LRUP.gxt AHU R C 32.8 AHUP.gxt AVU R C 32.8 AVUP.gxt LRD T C 32.8 LRDN.gxt -152 -151 -150.8 -150.7 -150.6 LLDN T C 32.8 LLDN.gxt -152 -151 -150.8 -150.7 -150.6 AHD T C 32.8 AHDN.gxt -150 -147.5 -145 -142.5 -142.1 AVD T C 32.8 AVDN.gxt -150 -147.5 -145 -142.5 -141.7 CMD R C 32.8 CMDG.pdf CMD R C 32.8 CMDW.pdf CMD R C 32.8 CMDO.pdf TLM T C 32.8 TLMG.pdf -168.7 -168.6 -168.5 -168.4 -168.3 TLM T C 32.8 TLMW.pdf -167.9 -167.8 -167.7 -167.6 -167.5 TLM T C 32.8 TLMO.pdf -174.1 -174 -173.9 -173.8 -173.7 UPC T C 32.8 UPCC.pdf -159.8 -159.7 -159.6 -159.5 -159.4 UPC T C 32.8 UPCK.pdf -157.3 -157.2 -157.1 -157 -156.9

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) 1CU 72000 R 5890 L C 1C 135.7 1CU LLUP 1CD LRDN 3CU 72000 R 5970 L C 3C 135.7 3CU LLUP 3CD LRDN 5CU 72000 R 6050 L C 5C 135.7 5CU LLUP 5CD LRDN 7CU 72000 R 6130 L C 7C 135.7 7CU LLUP 7CD LRDN 9CU 72000 R 6220 L C 9C 135.7 9CU LLUP 9CD LRDN 11CU 72000 R 6300 L C 11C 135.7 11CU LLUP 11CD LRDN 13CU 72000 R 6380 L C 13C 135.7 13CU LLUP 13CD LRDN 15CU 72000 R 6460 L C 2C 135.7 2CU LRUP 2CD LLDN 2CU 72000 R 5890 R C 4C 135.7 4CU LRUP 4CD LLDN 4CU 72000 R 5970 R C 6C 135.7 6CU LRUP 6CD LLDN 6CU 72000 R 6050 R C 8C 135.7 8CU LRUP 8CD LLDN 8CU 72000 R 6130 R C 10C 135.7 10CU LRUP 10CD LLDN 10CU 72000 R 6220 R C 12CD 135.7 12CU LRUP 12CD LLDN 12CU 72000 R 6300 R C 14CD 135.7 14CU LRUP 14CD LLDN 14CU 72000 R 6380 R C 1K 143.6 1KU AHUP 1KD AVDN 16CU 72000 R 6460 R C 3K 143.6 3KU AHUP 3KD AVDN 1KU 36000 R 14025 H C 5K 143.6 5KU AHUP 5KD AVDN 3KU 36000 R 14065 H C 7K 143.6 7KU AHUP 7KD AVDN 5KU 36000 R 14105 H C 9K 143.6 9KU AHUP 9KD AVDN 7KU 36000 R 14145 H C 11K 143.6 11KU AHUP 11KD AVDN 9KU 72000 R 14205 H C 13K 143.6 13KU AHUP 13KD AVDN 11KU 72000 R 14295 H C 15K 143.6 15KU AHUP 15KD AVDN 13KU 72000 R 14375 H C 2K 143.5 2KU AVUP 2KD AHDN 15KU 72000 R 14455 H C 4K 143.5 4KU AVUP 4KD AHDN 2KU 36000 R 14025 V C 6K 143.5 6KU AVUP 6KD AHDN 4KU 36000 R 14065 V C 8K 143.5 8KU AVUP 8KD AHDN 6KU 36000 R 14105 V C 10K 143.5 10KU AVUP 10KD AHDN 8KU 36000 R 14145 V C 12K 143.5 12KU AVUP 12KD AHDN 10KU 72000 R 14205 V C 14K 143.5 14KU AVUP 14KD AHDN 12KU 72000 R 14295 V C 16K 143.5 16KU AVUP 16KD AHDN

14KU 72000 R 14375 V C 11CK 140.1 11CU LLUP 11KD AVDN 16KU 72000 R 14455 V C 13CK 140.1 13CU LLUP 13KD AVDN 1CD 72000 T 3665 R C 15CK 140.1 15CU LLUP 15KD AVDN 3CD 72000 T 3745 R C 14CK 140 14CU LRUP 14KD AHDN 5CD 72000 T 3825 R C 16CK 140 16CU LRUP 16KD AHDN 7CD 72000 T 3905 R C 11KC 139.2 11KU AHUP 11CD LRDN 9CD 72000 T 3995 R C 13KC 139.2 13KU AHUP 13CD LRDN 11CD 72000 T 4075 R C 13CD 72000 T 4155 R C 2CD 72000 T 3655 L C 4CD 72000 T 3745 L C 6CD 72000 T 3825 L C 8CD 72000 T 3905 L C 10CD 72000 T 3995 L C 12CD 72000 T 4075 L C 14CD 72000 T 4155 L C 1KD 36000 T 10975 V C 3KD 36000 T 11015 V C 5KD 36000 T 11055 V C 7KD 36000 T 11095 V C 9KD 72000 T 11155 V C 11KD 72000 T 11495 V C 13KD 72000 T 11575 V C 15KD 72000 T 11655 V C 2KD 36000 T 10975 H C 4KD 36000 T 11015 H C 6KD 36000 T 11055 H C 8KD 36000 T 11095 H C 10KD 72000 T 11155 H C 12KD 72000 T 11495 H C 14KD 72000 T 11575 H C 16KD 72000 T 11655 H C CMD1 1000 R 6173.7 L T CMD2 1000 R 6176.3 L T TLM1 500 T 3947.5 R T TLM2 500 T 3952.5 R T UPC1 25 T 3950 V T UPC2 25 T 11198 R T UPC3 25 T 11452 R 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 72M0G7W 72000 4 49138 0.5 3.4 18.5 D2 10M3G7W 10300 4 6000 0.5 3.9 18.8 D3 100KG7W 100 4 64 0.5 3 18.2 D4 1M45G7W 1450 2 512 0.5 3.4 14.5 D5 400KG7W 400 2 128 0.5 3.4 14.5

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 PAL 15.6 1.5 10 23.4

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 13KC A1 2 36000 NEW DAWN S 4000 55.4 15.5 23.5 30 38 -154.1 31 1C 13KC D1 1 72000 NOTE.txt 55.4 15.5 23.5 34.2 42.2 -161.7 19.2 1C 13KC D2 4 10300 NOTE.txt 49.4 10.5 18.5 23.9 31.9 -162.5 21 1C 13KC D3 527 100 NOTE.txt 49.4 -9.9 -1.9 3.5 11.5 -163.4 21 1C 13KC A1 2 36000 NOTE.txt 4000 56.4 16.5 24.5 38.5 46.5 -145.6 32.6 1C 13KC D1 1 72000 NOTE.txt 56.4 16.5 24.5 42.7 50.7 -153.2 21.8 1C 13KC D2 4 10300 NOTE.txt 49.4 10.4 18.4 32.3 40.3 -154.1 24.5 1C 13KC D3 521 100 NOTE.txt 49.4 -9.9 -1.9 12 20 -154.9 24.5 1C 13KC A1 2 36000 NOTE.txt 4000 56.9 11.6 21.6 38.5 46.5 -145.6 32.6 1C 13KC D1 1 72000 NOTE.txt 56.9 13.6 23.6 42.7 50.7 -153.2 21.8 1C 13KC D2 5 10300 NOTE.txt 56.9 2.3 12.3 32.1 40.1 -154.3 24.5 1C 13KC D3 537 100 NOTE.txt 56.9 -17.9 -7.9 11.9 19.9 -155 24.5 1C 13KC D4 33 1450 NOTE.txt 56.9 -5.9 4.1 23.9 31.9 -155.1 24.5 1C 13KC D5 180 400 NOTE.txt 49 -9 1 12.9 20.9 -160.1 32.6 1C 13KC A1 2 36000 NOTE.txt 4000 56.9 13.1 23.1 30 38 -154.1 28.4 1C 13KC D1 1 72000 NOTE.txt 56.9 13.1 23.1 34.2 42.2 -161.7 19.2 1C 13KC D2 4 10300 NOTE.txt 56.9 3.2 13.2 24 32 -162.4 21 1C 13KC D3 481 100 NOTE.txt 56.9 -16.9 -6.9 3.9 11.9 -163 21

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 20008 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 202-944-7701 Remote Control (TT C) Location(s): S14a: Street Address: S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):

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 1278 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1722 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3000 23.6 0.811 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 578 4.9 0.838 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 31.1 8.5 0.68 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): 4818 4818 4818 4818 Bus (Watts): (b): (g): (l): (q): 372 307 372 307 Total (Watts): (c): (h): (m): (r): 5190 5125 5190 5125 Solar Array (Watts): (d): (i): (n): (s): 7420 6653 6946 6400 Depth of Battery (e) (j) (o) (t) Discharge (%): 45.1 % % 70.1 % % 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: 2010-11-04 11:58:17
Document Modified: 2010-11-04 11:58:17
© 2025 FCC.report
This site is not affiliated with or endorsed by the FCC