Attachment Schedule S Tech Data

This document pretains to SES-LIC-20050503-00526 for License on a Satellite Earth Station filing.

IBFS_SESLIC2005050300526_432578

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-1B 1/16/1998 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 5/13/1996 12 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 10/27/1997 32 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: 12/2/1997 1008 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) 13.75 G 14.50 G R Fixed Satellite Service 12.00 G 12.75 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: 150 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 Communications of Japan to N/S Station-Keeping provided (Optional): operate the satellite at the 150 degrees East Lontigude d. Toward West: Degrees E/W 0.05 Degrees Tolerance: orbital location. g. Westernmost: E e. Toward East: 0.05 Degrees 0.05 Degrees h. Easternmost: E 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) HAWAII BEAM E US Hawaii ASIAZONE BE E Asia JAPAN BEAM E Japan

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) HI-T T 41.8 21.8 0.1 0.3 30 N 90 HAWAII B 3.5 90 57.9 HI-R R 42.7 22.7 0.1 0.3 30 N 0 HAWAII B 7944 3.7 -96 31 1 HI-R2 R 42.7 22.7 0.1 0.3 30 N 90 HAWAII B 7944 3.7 -96 31 1 AS-T T 31.7 11.7 0.1 0.3 33 N 90 ASIAZON 1.6 90 47.9 AS-T T 31.7 11.7 0.1 0.3 33 N 0 ASIAZON 1.6 90 47.9 AS-R R 32.6 12.6 0.1 0.3 33 N 90 ASIAZON 661 4.4 -100 30 1 AS-R R 32.6 12.6 0.1 0.3 33 N 0 ASIAZON 661 4.4 -100 30 1 JP-T T 40.1 20.1 0.1 0.3 33 N 90 JAPAN BE 1.5 90 56.4 JP-T T 40.1 20.1 0.1 0.3 33 N 0 JAPAN BE 1.5 90 56.4 JP-R R 41 21 0.1 0.3 33 N 90 JAPAN BE 563 13.5 -100 30 1 JP-R R 41 32 0.1 0.3 33 N 0 JAPAN BE 563 13.5 -100 30 1 TTC- T 40.1 20.1 0.1 0.3 33 N 90 JAPAN BE 1.5 0.06 27.9 TTC- R 41 21 0.1 0.3 33 N 0 JAPAN BE 920 11.4 -110

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) HI-T T C 150 J1B_HI_TX.gxt -145.7 -145.5 -145.4 -145.3 -145.2 HI-R R C 150 J1B_HI_RX.gxt HI-R2 R C 150 HI-R2.PDF AS-T T C 150 AS-T1.PDF -156.1 -155.9 -155.8 -155.7 -155.6 AS-T T C 150 AS-T2.PDF -156.1 -155.9 -155.8 -155.7 -155.6 AS-R R C 150 AS-R1.PDF AS-R R C 150 AS-R2.PDF JP-T T C 150 JP-T1.PDF JP-T T C 150 JP-T2.PDF JP-R R C 150 JP-R1.PDF JP-R R C 150 JP-R2.PDF TTC- T C 150 TTC-T.PDF TTC- R C 150 TTC-R.PDF

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) EKR-1 36000 R 13774 H C EK-1 113 EKR-1 HI-R EKT-1 HI-T EKR-3 36000 R 13814 H C EK-3 113 EKR-3 HI-R EKT-3 HI-T EKR-5 36000 R 13854 H C EK-5 113 EKR-5 HI-R EKT-5 HI-T EKR-7 36000 R 13894 H C EK-7 113 EKR-7 HI-R EKT-7 HI-T EKT-1 36000 T 12026 V C K-1 117 KR-1 HI-R EKT-1 HI-T EKT-3 36000 T 12066 V C K-3 117 KR-3 HI-R EKT-3 HI-T EKT-5 36000 T 12106 V C K-5 117 KR-5 HI-R EKT-5 HI-T EKT-7 36000 T 12146 V C K-7 117 KR-7 HI-R EKT-7 HI-T KR-1 36000 R 14016 H C K-A1 128 KR-1 AS-R1 EKT-1 HI-T KR-2 36000 R 14036 V C K-A3 128 KR-3 AS-R1 EKT-3 HI-T KR-3 36000 R 14056 H C K-A5 128 KR-5 AS-R1 EKT-5 HI-T KR-4 36000 R 14076 V C K-A7 128 KR-7 AS-R1 EKT-7 HI-T KR-5 36000 R 14096 H C K-H1 116 EKR-1 HI-R KT-1 AS-T1 KR-6 36000 R 14116 V C K-H3 116 EKR-3 HI-R KT-3 AS-T1 KR-7 36000 R 14136 H C K-H5 116 EKR-5 HI-R KT-5 AS-T1 KR-8 36000 R 14156 V C K-H7 116 EKR-7 HI-R KT-7 AS-T1 KR-9 36000 R 14176 H C KR-10 36000 R 14196 V C KR-11 36000 R 14216 H C KR-12 36000 R 14236 V C KR-13 27000 R 14256 H C KR-14 27000 R 14271 V C KR-15 27000 R 14286 H C KR-16 27000 R 14301 V C KR-17 27000 R 14316 H C KR-18 27000 R 14331 V C KR-19 27000 R 14346 H C KR-20 27000 R 14361 V C KR-21 27000 R 14376 H C KR-22 27000 R 14391 V C

KR-23 27000 R 14406 H C KR-24 27000 R 14421 V C KR-25 27000 R 14436 H C KR-26 27000 R 14451 V C KR-27 27000 R 14466 H C KR-28 27000 R 14481 V C KT-1 36000 T 12268 V C KT-2 36000 T 12288 H C KT-3 36000 T 12308 V C KT-4 36000 T 12328 H C KT-5 36000 T 12348 V C KT-6 36000 T 12368 H C KT-7 36000 T 12388 V C KT-8 36000 T 12408 H C KT-9 36000 T 12428 V C KT-10 36000 T 12448 H C KT-11 36000 T 12468 V C KT-12 36000 T 12488 H C KT-13 27000 T 12508 V C KT-14 27000 T 12523 H C KT-15 27000 T 12538 V C KT-16 27000 T 12553 H C KT-17 27000 T 12568 V C KT-18 27000 T 12583 H C KT-19 27000 T 12598 V C KT-20 27000 T 12613 H C KT-21 27000 T 12628 V C KT-22 27000 T 12643 H C KT-23 27000 T 12658 V C KT-24 27000 T 12673 H C KT-25 27000 T 12688 V C KT-26 27000 T 12703 H C KT-27 27000 T 12718 V C KT-28 27000 T 12733 H 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) D2 520KG7W 520 4 512 0.75 7 16.3

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)

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) K-H1 K-H7 D2 69 520 SCHEDULE S 49.1 -0.6 0.6 24.8 26 -155.8 26.3 K-H1 K-H7 D2 56 520 SCHEDULE S 49.1 0.3 1.5 24 26.9 -154.9 26.3 K-A1 K-A7 D2 51 520 SCHEDULE S 49.1 -3.3 -0.9 36.8 37.3 -144.5 26.3 K-A1 K-A7 D2 69 520 SCHEDULE S 49.1 -1.6 -0.3 33.5 34 -147.8 26.3 EK-1 EK-7 D2 69 520 SCHEDULE S 49.1 -1.9 -0.7 34.2 34.7 -147.1 26.3

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): 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 1300 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1700 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3000 26 0.95 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 500 8 0.9 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 40 4 0.85 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): 3900 3900 3900 3900 Bus (Watts): (b): (g): (l): (q): 900 400 900 400 Total (Watts): (c): (h): (m): (r): 4800 4300 4800 4300 Solar Array (Watts): (d): (i): (n): (s): 5400 4800 5000 4500 Depth of Battery (e) (j) (o) (t) Discharge (%): 78 % % 78 % % 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: 2005-05-13 15:02:20
Document Modified: 2005-05-13 15:02:20
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