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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