Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20060908-00101 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2006090800101_526503

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: DIRECTV 9S 7/15/2006 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 11/1/2003 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 11/30/2005 22 0 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: 1/1/2006 6/30/2006 528 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) 17.3 G 17.8 G R Feeder Link for Broadcasting Satellite Service in FSS 12.2 G 12.7 G T Broadcasting Satellite Service - Video 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: 101.125 W 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) LABC S Area around Los Angeles, CA CRBC S Area around Castle Rock, CO USA S CONUS+Alaska+Hawaii SA1 S See GXT file associated with corresponding beam SA2 S See GXT file associated with corresponding beam SA3 S See GXT file associated with corresponding beam SA4 S See GXT file associated with corresponding beam SA5 S See GXT file associated with corresponding beam SA6 S See GXT file associated with corresponding beam SA7 S See GXT file associated with corresponding beam SA8 S See GXT file associated with corresponding beam SA9 S See GXT file associated with corresponding beam SA10 S See GXT file associated with corresponding beam SA11 S See GXT file associated with corresponding beam SA12 S See GXT file associated with corresponding beam SA13 S See GXT file associated with corresponding beam SA14 S See GXT file associated with corresponding beam SA15 S See GXT file associated with corresponding beam SA16 S See GXT file associated with corresponding beam SA17 S See GXT file associated with corresponding beam SA18 S See GXT file associated with corresponding beam SA19 S See GXT file associated with corresponding beam SA20 S See GXT file associated with corresponding beam SA21 S See GXT file associated with corresponding beam SA22 S See GXT file associated with corresponding beam SA23 S See GXT file associated with corresponding beam SA24 S See GXT file associated with corresponding beam SA25 S See GXT file associated with corresponding beam SA26 S See GXT file associated with corresponding beam

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) UL1 R 46 45 0.14 27 Y LABC 9332 6.3 -100 31 1 UL2 R 50.4 49.4 0.14 27 Y CRBC 12589 9.4 -100 31 1 N101 T 38.3 30.3 0.14 27 N USA 2.4 302 60.1 RB01 T 49.9 45.9 0.05 27 N SA1 1.5 15.8 60.4 RB02 T 50.5 46.5 0.05 27 N SA2 1.4 14.1 60.6 BB03 T 48.5 44.5 0.05 27 N SA3 2.4 28.8 60.7 RB04 T 50.7 46.7 0.05 27 N SA4 2.8 12.6 58.9 RB05 T 50.7 46.7 0.05 27 N SA5 2.1 5.8 56.2 RB06 T 50.5 46.5 0.05 27 N SA6 2.6 23.4 61.6 BB07 T 48.1 44.1 0.05 27 N SA7 1.8 4 52.3 BB08 T 48.3 44.3 0.05 27 N SA8 2.3 19.1 58.8 BB09 T 44.7 40.7 0.05 27 N SA9 2.3 10.7 52.7 BB10 T 47.6 43.6 0.05 27 N SA10 2.8 12.6 55.8 BB11 T 47.3 43.3 0.05 27 N SA11 2.7 12.6 55.6 CB12 T 49.9 45.9 0.05 27 N SA12 2.2 42.7 64 CB13 T 50.2 46.2 0.05 27 N SA13 2.6 19.1 60.4 CB14 T 49.8 45.8 0.05 27 N SA14 2.5 34.7 62.7 CB15 T 50.5 46.5 0.05 27 N SA15 2.8 17.8 60.2 CB16 T 49 45 0.05 27 N SA16 2.6 7.1 54.9 CB17 T 48.1 44.1 0.05 27 N SA17 2.7 3.6 51 CB18 T 50.2 46.2 0.05 27 N SA18 2.7 22.4 61 CB19 T 47.6 43.6 0.05 27 N SA19 1.5 5.6 53.6 CB20 T 48.9 44.9 0.05 27 N SA20 2.3 5.8 54.2 BB21 T 48.2 44.2 0.05 27 N SA21 2.5 11 56.1 BB22 T 47.5 43.7 0.05 27 N SA22 2.6 18.6 57.6 BB23 T 47.7 43.7 0.05 27 N SA23 1.7 11.2 56.5 BB24 T 47.7 43.7 0.05 27 N SA24 1.8 7.2 54.5 RB25 T 48.2 44.2 0.05 27 N SA25 1.6 5.4 53.9 RB26 T 45.2 41.2 0.05 27 N SA26 1.6 11 54

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) N101 T C -101 N101_C.gxt RB01 T C -101 RB01_C.gxt RB02 T C -101 RB02_C.gxt BB03 T C -101 BB03_C.gxt RB04 T C -101 RB04_C.gxt RB05 T C -101 RB05_C.gxt RB06 T C -101 RB06_C.gxt BB07 T C -101 BB07_C.gxt BB08 T C -101 BB08_C.gxt BB09 T C -101 BB09_C.gxt BB10 T C -101 BB10_C.gxt BB11 T C -101 BB11_C.gxt CB12 T C -101 CB12_C.gxt CB13 T C -101 CB13_C.gxt CB14 T C -101 CB14_C.gxt CB15 T C -101 CB15_C.gxt CB16 T C -101 CB16_C.gxt CB17 T C -101 CB17_C.gxt CB18 T C -101 CB18_C.gxt CB19 T C -101 CB19_C.gxt CB20 T C -101 CB20_C.gxt BB21 T C -101 BB21_C.gxt BB22 T C -101 BB22_C.gxt BB23 T C -101 BB23_C.gxt BB24 T C -101 BB24_C.gxt RB25 T C -101 RB25_C.gxt RB26 T C -101 RB26_C.GXT UL1 R C -101 ULLA_C.gxt

UL2 R C -101 ULCR_C.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) R0001 24000 R 17324 R C NAT2 107 R0002 UL1 T0002 DL1 R0003 24000 R 17353.16 R C NAT6 107 R0006 UL1 T0006 DL1 R0005 24000 R 17382.32 R C NAT8 107 R0008 UL1 T0008 DL1 R0007 24000 R 17411.48 R C NAT10 107 R0010 UL1 T0010 DL1 R0009 24000 R 17440.64 R C NAT14 107 R0014 UL1 T0014 DL1 R0011 24000 R 17469.8 R C NAT16 107 R0016 UL1 T0016 DL1 R0013 24000 R 17498.96 R C NAT22 107 R0022 UL1 T0022 DL1 R0015 24000 R 17528.12 R C NAT24 107 R0024 UL1 T0024 DL1 R0017 24000 R 17557.28 R C NAT30 107 R0030 UL1 T0030 DL1 R0019 24000 R 17586.44 R C NAT32 107 R0032 UL1 T0032 DL1 R0021 24000 R 17615.6 R C S1 102 R0027 UL2 T0028 RB01 R0023 24000 R 17644.76 R C S2 102 R0029 UL2 T0028 RB02 R0025 24000 R 17673.92 R C S3 102 R0021 UL1 T0020 BB03 R0027 24000 R 17703.08 R C S3A 102 R0029 UL1 T0028 BB03 R0029 24000 R 17732.24 R C S4 102 R0031 UL2 T0028 RB04 R0031 24000 R 17761.4 R C S5 102 R0018 UL2 T0018 RB05 R0002 24000 R 17338.58 L C S5A 102 R0028 UL2 T0028 RB05 R0004 24000 R 17367.74 L C S6 102 R0007 UL2 T0018 RB06 R0006 24000 R 17396.9 L C S6A 102 R0017 UL2 T0028 RB06 R0008 24000 R 17426.06 L C S7 102 R0031 UL1 T0028 BB07 R0010 24000 R 17455.22 L C S8 102 R0027 UL1 T0028 BB08 R0012 24000 R 17484.38 L C S9 102 R0005 UL2 T0004 BB09 R0014 24000 R 17513.54 L C S9A 102 R0013 UL2 T0012 BB09 R0016 24000 R 17542.7 L C S10 102 R0007 UL1 T0018 BB10 R0018 24000 R 17571.86 L C S10A 102 R0017 UL1 T0028 BB10 R0020 24000 R 17601.02 L C S11 102 R0018 UL1 T0018 BB11 R0022 24000 R 17630.18 L C S11A 102 R0028 UL1 T0028 BB11 R0024 24000 R 17659.34 L C S12 102 R0004 UL2 T0004 CB12 R0026 24000 R 17688.5 L C S12A 102 R0012 UL2 T0012 CB12 R0028 24000 R 17717.66 L C S12B 102 R0020 UL2 T0020 CB12

R0030 24000 R 17746.82 L C S13 102 R0003 UL2 T0004 CB13 R0032 24000 R 17775.98 L C S13A 102 R0011 UL2 T0012 CB13 T0002 24000 T 12238.58 L C S13B 102 R0019 UL2 T0020 CB13 T0004 24000 T 12267.74 L C S14 102 R0003 UL1 T0004 CB14 T0006 24000 T 12296.9 L C S14A 102 R0011 UL1 T0012 CB14 T0008 24000 T 12326.06 L C S14B 102 R0019 UL1 T0020 CB14 T0010 24000 T 12355.22 L C S15 102 R0013 UL1 T0012 CB15 T0012 24000 T 12384.38 L C S15A 102 R0015 UL1 T0026 CB15 T0014 24000 T 12413.54 L C S16 102 R0001 UL2 T0012 CB16 T0016 24000 T 12442.7 L C S16A 102 R0009 UL2 T0020 CB16 T0018 24000 T 12471.86 L C S17 102 R0023 UL2 T0020 CB17 T0020 24000 T 12501.02 L C S18 102 R0001 UL1 T0012 CB18 T0022 24000 T 12530.18 L C S18A 102 R0009 UL1 T0020 CB18 T0024 24000 T 12559.34 L C S19 102 R0023 UL1 T0020 CB19 T0026 24000 T 12588.5 L C S20 102 R0004 UL1 T0004 CB20 T0028 24000 T 12617.66 L C S20A 102 R0012 UL1 T0012 CB20 T0030 24000 T 12646.82 L C S20B 102 R0020 UL1 T0020 CB20 T0032 24000 T 12675.98 L C S21 102 R0021 UL2 T0018 BB21 CMD1 1000 R 17795 R T S21A 102 R0015 UL2 T0026 BB21 TLM1 1000 T 12695.5 R T S22 102 R0025 UL2 T0026 BB22 TLM2 1000 T 12696.5 R T S23 102 R0026 UL2 T0026 BB23 S24 102 R0005 UL1 T0004 BB24 S25 102 R0026 UL1 T0026 RB25 S26 102 R0025 UL1 T0026 RB26 T1 TLM1 N101 T2 TLM2 N101

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) BSS1 24M0G7W 24000 8 43550 0.7258 8.2 28 BSS2 24M0G7W 24000 4 30320 0.758 6.8 28

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) CMD 1M00F9D 1000 1 7.6 28 TLM 1M00F9D 1000 1 7.6 28

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) NAT2 NAT32 BSS1 1 63 9.7 14.7 60.1 60.1 13 NAT2 NAT32 BSS2 1 63 9.7 14.7 60.1 60.1 13 S1 S26 BSS1 1 63 9.7 14.7 52.3 61.6 13 S1 S26 BSS2 1 63 9.7 14.7 52.3 61.6 13 T1 T2 TLM 1 19.2 19.2 29.3

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: 1600 Forbes Way S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Long Beach Los Angeles CA 90810 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 310-525-5590 Remote Control (TT C) Location(s): S14a: Street Address: 33E Telegraph Rd. S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Fillmore Ventura CA 93015 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 805-524-4444

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 2364 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3140 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5685 31.3 0.85 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 984 12.1 0.84 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 59.6 7.5 0.73 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): 7581 7581 7581 7581 Bus (Watts): (b): (g): (l): (q): 2845 1788 2845 1788 Total (Watts): (c): (h): (m): (r): 10696 9639 10696 9639 Solar Array (Watts): (d): (i): (n): (s): 12710 11442 11820 10641 Depth of Battery (e) (j) (o) (t) Discharge (%): 80 % 0 % 80 % 0 % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: YES NO X 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: 2006-09-11 13:14:17
Document Modified: 2006-09-11 13:14:17
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