Attachment Schedule S Tech Data

This document pretains to SES-MFS-20060720-01217 for Modification w/ Foreign Satellite (earth station) on a Satellite Earth Station filing.

IBFS_SESMFS2006072001217_512118

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: JCSAT-5A 6/30/2006 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 12 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 1/20/2006 40 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: 4/12/2006 2584 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) 12.254 G 12.749 G T Fixed Satellite Service 14.002 G 14.497 G R Fixed Satellite Service 3.702 G 4.118 G T Fixed Satellite Service 5.927 G 6.343 G R 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: 132 E JSAT Corporation has authorization from Ministry of Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Internal Affairs and Communication of Japan to N/S Station-Keeping provided (Optional): operate the satellite at the 132 degrees East longtitude d. Toward West: Degrees E/W 0.05 Degrees Tolerance: orbital location. 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) C BAND E Asia & Hawaii KU BAND E Japan & Asia

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) C-T- T 26.2 16.2 0.1 0.3 27 N 0 C BAND 2 45 40.7 C-R- R 29.2 19.2 0.1 0.3 27 N 0 C BAND 537 1.8 -97 15 1 C-T- T 26.1 16.1 0.1 0.3 27 N 90 C BAND 2 45 40.6 C-R- R 29.2 19.2 0.1 0.3 27 N 90 C BAND 537 1.8 -97 15 1

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) C-T- T C 132 JCSAT-5A_CTH.gxt -152 -149.5 -147 -144.5 -142 C-R- R C 132 JCSAT-5A_CRH.gxt C-T- T C 132 JCSAT-5A_CTV.gxt -152 -149.5 -147 -144.5 -142 C-R- R C 132 JCSAT-5A_CRV.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) C1T 36000 T 3.72 V C C1 114 C1R C-R-H C1T C-T-V C1R 36000 R 5.945 H C C2 114 C2R C-R-V C2T C-T-H C2T 36000 T 3.74 H C C3 114 C3R C-R-H C3T C-T-V C2R 36000 R 5.965 V C C4 114 C4R C-R-V C4T C-T-H C3T 36000 T 3.76 V C C5 114 C5R C-R-H C5T C-T-V C3R 36000 R 5.985 H C C6 114 C6R C-R-V C6T C-T-H C4T 36000 T 3.78 H C C7 114 C7R C-R-H C7T C-T-V C4R 36000 R 6.005 V C C8 114 C8R C-R-V C8T C-T-H C5T 36000 T 3.80 V C C9 114 C9R C-R-H C9T C-T-V C5R 36000 R 6.025 H C C10 114 C10R C-R-V C10T C-T-H C6T 36000 T 3.82 H C C11 114 C11R C-R-H C11T C-T-V C6R 36000 R 6.045 V C C12 114 C12R C-R-V C12T C-T-H C7T 36000 T 3.84 V C C13 114 C13R C-R-H C13T C-T-V C7R 36000 R 6.065 H C C14 114 C14R C-R-V C14T C-T-H C8T 36000 T 3.86 H C C15 114 C15R C-R-H C15T C-T-V C8R 36000 R 6.085 V C C16 114 C16R C-R-V C16T C-T-H C9T 36000 T 3.88 V C C17 114 C17R C-R-H C17T C-T-V C9R 36000 R 6.105 H C C18 114 C18R C-R-V C18T C-T-H C10T 36000 T 3.90 H C C19 114 C19R C-R-H C19T C-T-V C10R 36000 R 6.125 V C C20 114 C20R C-R-V C20T C-T-H C11T 36000 T 3.92 V C C11R 36000 R 6.145 H C C12T 36000 T 3.94 H C C12R 36000 R 6.165 V C C13T 36000 T 3.96 V C C13R 36000 R 6.185 H C C14T 36000 T 3.98 H C C14R 36000 R 6.205 V C C15T 36000 T 4.00 V C C15R 36000 R 6.225 H C

C16T 36000 T 4.02 H C C16R 36000 R 6.245 V C C17T 36000 T 4.04 V C C17R 36000 R 6.265 H C C18T 36000 T 4.06 H C C18R 36000 R 6.285 V C C19T 36000 T 4.08 V C C19R 36000 R 6.305 H C C20T 36000 T 4.10 H C C20R 36000 R 6.325 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 273KG7W 573 8 512 0.75 0 10.3 23

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)

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) C1 C1 D1 65 18.5 54.3 24.8 27 34.7 38.7 -123.8

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): No Remote Control (TT C) Location(s): S14a: Street Address: 229-1 Miho-cho S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Yokohama Kanagawa 226-0015 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): +81-45-922-7111

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 2226 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1528 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4410 26.4 0.801 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 656 14.3 0.827 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 70.6 8.3 0.663 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): 8605 8605 8605 8605 Bus (Watts): (b): (g): (l): (q): 510 494 550 534 Total (Watts): (c): (h): (m): (r): 9115 9099 9155 9139 Solar Array (Watts): (d): (i): (n): (s): 14452 12790 12115 10832 Depth of Battery (e) (j) (o) (t) Discharge (%): 72.4 % 72.4 % 72.6 % 72.6 % 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: 2006-07-21 12:57:19
Document Modified: 2006-07-21 12:57:19
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