Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20071221-00182 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2007122100182_618871

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: SBS 6 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: 19 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: 817 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) 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: 80.9 W Meet customer requirements 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 0.3 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 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) KHU R 36.9 26.9 0.27 0.18 01 9.2 -84.2 14 2 KVUL R 36.9 26.9 0.27 0.18 90 1 9.2 -84.2 14 2 KHD T 36.6 26.6 0.27 0.18 0 1 50.9 KVDL T 36.6 26.6 0.27 0.18 90 1 50.9 OCM R 0.5 -1.5 0.27 0.18 0 2 -37.2 -88 RCM R 42.5 32.5 0.27 0.18 90 1 -2.9 -122 OTL T 1.6 -0.4 0.27 0.18 90 2 12.4 RTL T 36.6 26.6 0.27 0.18 01 21.6

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) KHU R C -80.9 khul.gxt KVUL R C -80.9 kvul.gxt KHD T C -80.9 khdl.gxt KVDL T C -80.9 kvdl.gxt OCM R C -80.9 ocmd.gxt RCM R C -80.9 RCMD.pdf OTL T C -80.9 otlm.gxt RTL T C -80.9 rtlm.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) KU001 43000 R 14025 V C K1 106.1 KU001 KVUL KD001 KHDL KU003 43000 R 14074 V C K0001 106.1 KU001 KVUL KD001 KHDL KU005 43000 R 14123 V C K0003 106.1 KU003 KVUL KD003 KHDL KU007 43000 R 14172 V C K0005 106.1 KU005 KVUL KD005 KHDL KU009 43000 R 14221 V C K0007 106.1 KU007 KVUL KD007 KHDL KU011 43000 R 14270 V C K0009 106.1 KU009 KVUL KD009 KHDL KU013 43000 R 14319 V C K0011 106.1 KU011 KVUL KD011 KHDL KU015 43000 R 14368 V C K0013 106.1 KU013 KVUL KD013 KHDL KU017 43000 R 14417 V C K0015 106.1 KU015 KVUL KD015 KHDL KU019 43000 R 14466 V C K0017 106.1 KU017 KVUL KD017 KHDL KU002 43000 R 14049.5 H C K0019 106.1 KU019 KVUL KD019 KHDL KU004 43000 R 14098.5 H C K0002 106.1 KU002 KHUL KD002 KVDL KU006 43000 R 14147.5 H C K0004 106.1 KU004 KHUL KD004 KVDL KU008 43000 R 14196.5 H C K0006 106.1 KU006 KHUL KD006 KVDL KU010 43000 R 14245.5 H C K0008 106.1 KU008 KHUL KD008 KVDL KU012 43000 R 14294.5 H C K0010 106.1 KU010 KHUL KD010 KVDL KU014 43000 R 14343.5 H C K0012 106.1 KU012 KHUL KD012 KVDL KU016 43000 R 14392.5 H C K0014 106.1 KU014 KHUL KD014 KVDL KU018 43000 R 14441.5 H C K0016 106.1 KU016 KHUL KD016 KVDL KD001 43000 T 11725 H C K0018 106.1 KU018 KHUL KD018 KVDL KD003 43000 T 11774 H C KD005 43000 T 11823 H C KD007 43000 T 11872 H C KD009 43000 T 11921 H C KD011 43000 T 11970 H C KD013 43000 T 12019 H C KD015 43000 T 12068 H C KD017 43000 T 12117 H C KD019 43000 T 12166 H C KD002 43000 T 11749.5 V C

KD004 43000 T 11798.5 V C KD006 43000 T 11847.5 V C KD008 43000 T 11896.5 V C KD010 43000 T 11945.5 V C KD012 43000 T 11994.5 V C KD014 43000 T 12043.5 V C KD016 43000 T 12092.5 V C KD018 43000 T 12141.5 V C CMD1 6000 R 14003.0 H T CMD2 6000 R 14497.0 V T TLM1 1000 T 12195 V T TLM2 1000 T 12198 V T TLM3 1000 T 12195 H T TLM4 1000 T 12198 H 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 30M8G7W 30800 4 28380 0.5 5.2 13.4 D2 6M77G7W 6771.1 4 6000 0.5 3.9 14.1 D3 75K4G7W 75.4 4 64 0.5 3 13.4 D4 1M23G7W 1229 2 512 0.5 3.4 13.3 D5 307KG7W 307 2 128 0.5 3.4 13.3

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 17.8

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) K1 K0019 A1 1 Link_Budgets.p 4000 58.1 13 23 32.5 42.5 -149.6 41.9 K1 K0019 D1 1 Link_Budgets.p 56.9 8.6 18.6 34.8 44.8 -156.2 33.1 K1 K0019 D2 4 10300 Link_Budgets.p 56.9 4.5 14.5 28.1 38.1 -156.3 33.1 K1 K0019 D3 430 100 Link_Budgets.p 56.9 -15.7 -5.7 7.9 17.9 -157 33.1 K1 K0019 D4 29 1450 Link_Budgets.p 56.9 -3.7 6.3 19.9 29.9 -157.1 33.1 K1 K0019 D5 107 400 Link_Budgets.p 56.9 -9.7 0.3 13.9 23.9 -157.1 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): #Error

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: 2008-01-30 13:27:11
Document Modified: 2008-01-30 13:27:11
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC