Attachment Schedule S Tech Data

This document pretains to SAT-PPL-20040805-00157 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2004080500157_386754

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: SUPERBIRD-C N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 12 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 24 MHz d. Estimated Launch Date: h. Total Transponder Bandwidth (no. transponders x Bandwidth) l. Orbit Type: Mark all boxes that apply: 7/28/1997 792 MHz GSO NGSO 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) 14 G 14.5 G R Fixed Satellite Service 11.902 G 11.938 G T Fixed Satellite Service 11.9895 G 12.0165 G T Fixed Satellite Service 12.0495 G 12.0765 G T Fixed Satellite Service 12.1095 G 12.1365 G T Fixed Satellite Service 12.25 G 12.75 G 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: 143.95 E This position was granted by Japanese Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be administration.Under this application, we are only N/S Station-Keeping provided (Optional): seeking authority to provide service to the U.S. d. Toward West: Degrees Degrees E/W 0.05 Tolerance: territories in this bands(14-14.5 GHz and 11.7-12.5 g. Westernmost: e. Toward East: 0.05 Degrees GHz). 0.1 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 SA_1.gxt J,USA

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 Flux Density (Y/N) Value Size (dB) (dBW) Temp (k) Pt. (dBW/m2) JHR R 40 25 0.1 0 33 N 12 1 457 13.4 -108 30 1 JHR R 40 25 0.1 0 33 N -78 1 457 13.4 -108.6 30 1 HTH T 41.6 38.4 0.1 0 30 N -78 1 1.8 17.8 52.3 JTV T 41.6 26.6 0.1 0 33 N 12 1 1.6 63.1 58 JTH T 41.6 26.6 0.1 0 33 N -78 1 1.6 63.1 58

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) JHR R C 143.95 JHRH_C.PDF JHRH.gxt JHR R X 143.95 JHRH_X.PDF JHRH_X.gxt JHR R C 143.95 JHRV_C.PDF JHRV.gxt JHR R X 143.95 JHRV_X.PDF JHRV_X.gxt JTV T C 143.95 JTV_C.PDF JTV.gxt JTV T X 143.95 JTV_X.PDF JTV_X.gxt JTH T C 143.95 JTH_C.PDF JTH.gxt JTH T X 143.95 JTH_X.PDF JTH_X.gxt HTH T C 143.95 HTH_C.PDF HTH.gxt HTH T X 143.95 HTH_X.PDF HTH_X.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) (c) (d) Center (e) (f) TTC (a) (b) Receive Band Transmit Band Channel Assigned T/R Frequency Polarization or Comm Transponder Transponder (c) Channel (d) Beam (e) Channel (f) Beam ID No. Bandwidth Mode (MHz) (H, V, L, R) Channel ID Gain (dB) No. ID No. (kHz) (T or C) T1 54000 T 12320 H C 1 133.7 R1 JHRH T1 JTV T2 54000 T 12380 H C 2 133.7 R2 JHRH T2 JTV T3 36000 T 12430 H C 3 133.7 R3 JHRH T3 JTV T4 36000 T 11920 H C 4 133.7 R4 JHRH T4 HTH T5 27000 T 12523 H C 5 133.7 R5 JHRH T5 JTV T6 27000 T 12003 H C 6 133.7 R6 JHRH T6 HTH T7 27000 T 12583 H C 7 133.7 R7 JHRH T7 JTV T8 27000 T 12063 H C 8 133.7 R8 JHRH T8 HTH T9 27000 T 12643 H C 9 133.7 R9 JHRH T9 JTV T10 27000 T 12123 H C 10 133.7 R10 JHRH T10 HTH T11 27000 T 12703 H C 11 133.7 R11 JHRH T11 JTV T12 27000 T 12733 H C 12 133.7 R12 JHRH T12 JTV T13 54000 T 12320 V C 13 133.7 R13 JHRV T13 JTH T14 54000 T 12380 V C 14 133.7 R14 JHRV T14 JTH T15 36000 T 12430 V C 15 133.7 R15 JHRV T15 JTH T16 36000 T 12470 V C 16 133.7 R16 JHRV T16 JTH T17 27000 T 12508 V C 17 133.7 R17 JHRV T17 JTH T18 27000 T 12538 V C 18 133.7 R18 JHRV T18 JTH T19 27000 T 12568 V C 19 133.7 R19 JHRV T19 JTH T20 27000 T 12598 V C 20 133.7 R20 JHRV T20 JTH T21 27000 T 12628 V C 21 133.7 R21 JHRV T21 JTH T22 27000 T 12658 V C 22 133.7 R22 JHRV T22 JTH T23 27000 T 12688 V C 23 133.7 R23 JHRV T23 JTH T24 27000 T 12718 V C 24 133.7 R24 JHRV T24 JTH R1 54000 R 14050 V C R2 54000 R 14110 V C R3 36000 R 14160 V C R4 36000 R 14200 V C R5 27000 R 14253 V C R6 27000 R 14283 V C

R7 27000 R 14313 V C R8 27000 R 14343 V C R9 27000 R 14373 V C R10 27000 R 14403 V C R11 27000 R 14433 V C R12 27000 R 14463 V C R13 54000 R 14050 H C R14 54000 R 14110 H C R15 36000 R 14160 H C R16 36000 R 14200 H C R17 27000 R 14238 H C R18 27000 R 14268 H C R19 27000 R 14298 H C R20 27000 R 14328 H C R21 27000 R 14358 H C R22 27000 R 14388 H C R23 27000 R 14418 H C R24 27000 R 14448 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) 1 76K8G7W 100 4 64 0.5 5.7 17.9 2 615KG7W 750 4 512 0.5 5.7 17.9 3 2M46G7W 2900 4 2048 0.5 5.7 17.9 4 7M38G7W 9000 4 8493 0.75 6.8 19 5 14M8G7W 18000 8 22648 0.6666667 10.5 22.7 6 26M9G7W 36000 8 41227 0.6666667 11.5 23.7 7 35M8G7W 36000 4 41227 0.75 7.4 19.6

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. Bandwidth per Carrier NTSC, Weighting SCPC/FM Preemphasis, Objective Objective Companded Baseband Baseband Modulation ID (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) 1 24 1 360 LINK_BUDGET 46.5 3.9 13.9 27.2 36.4 24.2 1 24 2 48 LINK_BUDGET 46.5 12.7 22.7 36 44.2 24.2 1 24 3 16 LINK_BUDGET 46.5 15.4 15.4 38.8 49.1 24.2 1 24 4 12 LINK_BUDGET 46.5 22.6 22.6 45.8 53.8 30.4 1 24 5 4 LINK_BUDGET 55.7 20.4 20.4 49.5 56 30.4 1 24 6 2 LINK_BUDGET 58.8 20.2 20.2 52.8 56 34.6 1 24 7 1 LINK_BUDGET 58.8 20.2 20.2 52.8 56 34.6 4 10 1 360 LINK_BUDGET 58.8 20.2 8.6 52.8 56 34.6 4 10 2 48 LINK_BUDGET 46.5 -2.7 7.3 31.5 37.5 24.2 4 10 3 16 LINK_BUDGET 46.5 2 12 36.2 41.4 24.2 4 10 4 12 LINK_BUDGET 55.7 2.9 12.9 42.3 48.1 30.4 4 10 5 4 LINK_BUDGET 55.7 5.9 15.9 45.3 51 30.4 4 10 6 2 LINK_BUDGET 58.8 5.8 15.8 48.3 51 34.6 4 4 7 1 LINK_BUDGET 58.8 5.8 15.8 48.3 51 34.6

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: Oomiya-kogyodanchi 60 S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Ibaraki 319-2143 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 81295524111 Remote Control (TT C) Location(s): S14a: Street Address: 3-1,ogi-cyo S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Yamaguchi 753-0002 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 81839213220

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 1416 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1673 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3089 26.2 0.85 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 439 2.6 0.8 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 44 8.2 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): 3919 3919 3919 3919 Bus (Watts): (b): (g): (l): (q): 291 275 291 275 Total (Watts): (c): (h): (m): (r): 4209 4194 4209 4194 Solar Array (Watts): (d): (i): (n): (s): 5470 4844 5002 4557 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 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: 2004-08-05 12:13:32
Document Modified: 2004-08-05 12:13:32
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