Attachment Schedule S Tech Data

This document pretains to SES-MFS-20090106-00002 for Modification w/ Foreign Satellite (earth station) on a Satellite Earth Station filing.

IBFS_SESMFS2009010600002_694029

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-2A N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 11 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 26 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: 3/29/2002 1344 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: 154 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 154 degrees East longitude 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

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) CVT T 24.9 9.9 0.1 0.3 30 N 90 C BAND 1.8 34 38.4 CHR R 26.5 11.5 0.1 0.3 30 N 0 C BAND 537 -0.4 -98.2 15 0.5 KVT T 39.6 29.6 0.1 0.3 33 N 90 KU BAND 1.5 120 58.9 KVR R 39.9 29.9 0.1 0.3 33 N 90 KU BAND 490 12.9 -109 20 1 KHT T 39.3 29.3 0.1 0.3 33 N 0 KU BAND 1.5 120 58.6 KHR R 39.6 29.6 0.1 0.3 33 N 0 KU BAND 490 12.7 -108.8 20 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) CVT T C 154 JCSAT-2R_CVT.gxt -164.4 -164.3 -164.2 -164.1 -164 CHR R C 154 JCSAT-2A_CHR.gxt KVT T C 154 JCSAT-2A_KVT.gxt -200 -200 -200 -200 -200 KVR R C 154 JCSAT-2A_KVR.gxt KHT T C 154 JCSAT-2A_KHT.gxt -200 -200 -200 -200 -200 KHR R C 154 JCSAT-2A_KHR.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) C3T 36000 T 3720 V C C3 113.4 C3R CHR C3T CVT C3R 36000 R 5945 H C C5 113.4 C5R CHR C5T CVT C5T 36000 T 3760 V C C7 113.4 C7R CHR C7T CVT C5R 36000 R 5985 H C C9 113.4 C9R CHR C9T CVT C7T 36000 T 3800 V C C11 113.4 C11R CHR C11T CVT C7R 36000 R 6025 H C C13 113.4 C13R CHR C13T CVT C9T 36000 T 3840 V C C15 113.4 C15R CHR C15T CVT C9R 36000 R 6065 H C C17 113.4 C17R CHR C17T CVT C11T 36000 T 3880 V C C19 113.4 C19R CHR C19T CVT C11R 36000 R 6105 H C C21 113.4 C21R CHR C21T CVT C13T 36000 T 3920 V C K1 124.9 K1R KHR K1T KVT C13R 36000 R 6145 H C K2 124.9 K2R KVR K2T KHT C15T 54000 T 3990 V C K3 124.9 K3R KHR K3T KVT C15R 54000 R 6215 H C K4 124.9 K4R KVR K4T KHT C17T 54000 T 4050 V C K5 124.9 K5R KHR K5T KVT C17R 54000 R 6275 H C K6 124.9 K6R KVR K6T KHT C19T 54000 T 4110 V C K7 124.9 K7R KHR K7T KVT C19R 54000 R 6335 H C K8 124.9 K8R KVR K8T KHT C21T 54000 T 4170 V C K9 124.9 K9R KHR K9T KVT C21R 54000 R 6395 H C K10 124.9 K10R KVR K10T KHT K1T 57000 T 12283.25 V C K11 124.9 K11R KHR K11T KVT K1R 57000 R 14031.25 H C K12 124.9 K12R KVR K12T KHT K2T 57000 T 12298.25 H C K13 124.9 K13R KHR K13T KVT K2R 57000 R 14046.25 V C K14 124.9 K14R KVR K14T KHT K3T 57000 T 12343.25 V C K15 124.9 K15R KHR K15T KVT K3R 57000 R 14091.25 H C K16 124.9 K16R KVR K16T KHT K4T 57000 T 12358.25 H C K4R 57000 R 14106.25 V C K5T 57000 T 12403.25 V C K5R 57000 R 12451.25 H C

K6T 57000 T 12418.25 H C K6R 57000 R 14166.25 V C K7T 57000 T 12463.25 V C K7R 57000 R 14211.25 H C K8T 57000 T 12478.25 H C K8R 57000 R 14226.25 V C K9T 57000 T 12523.25 V C K9R 57000 R 14271.25 H C K10T 57000 T 12538.25 H C K10R 57000 R 14286.25 V C K11T 57000 T 12583.25 V C K11R 57000 R 14331.25 H C K12T 57000 T 12598.25 H C K12R 57000 R 14346.25 V C K13T 57000 T 12643.25 V C K13R 57000 R 14391.25 H C K14T 57000 T 12658.25 H C K14R 57000 R 14406.25 V C K15T 57000 T 12703.25 V C K15R 57000 R 14451.25 H C K16T 57000 T 12718.25 H C K16R 57000 R 14466.25 V C C-BCN T 4199.375 H T KUBCN T 12247.5 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 2M99G7W 3000 4 3072 0.75 0 5.8 13.7 D2 787KG7W 790 4 768 0.75 0 5.8 13.7

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) C3 C13 D1 12 3000 51 20 27.8 -174.3 28 C3 C13 D2 45 790 51 20 27.8 -174.3 28 C15 C21 D1 12 3000 51 20 27.8 -174.3 28 C15 C21 D2 45 790 51 20 27.8 -174.3 28

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 Remote Control (TT C) Location(s): S14a: Street Address: 229-1 Miho-cho S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Yokohama japan 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 1143.6 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 944.2 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2415.4 21 0.9191 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 327.6 7.6 0.8903 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 32.9 4.3 0.81477 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): 2611 2611 2611 2611 Bus (Watts): (b): (g): (l): (q): 418 387 418 387 Total (Watts): (c): (h): (m): (r): 3029 2998 3029 2998 Solar Array (Watts): (d): (i): (n): (s): 4048 3653 3557 3297 Depth of Battery (e) (j) (o) (t) Discharge (%): 78 % 78 % 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? X 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? 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: 2009-02-03 15:37:16
Document Modified: 2009-02-03 15:37:16
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