Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20041008-00196 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2004100800196_401281

 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:
  ECHOSTAR-117W                                                                                                                               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:
                                                                           64                                                                 0                                            MHz

d. Estimated Launch Date:                                                h. Total Transponder Bandwidth (no. transponders x Bandwidth)      l. Orbit Type: Mark all boxes that apply:
                                                                           7360                                          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)
28.35                  G           28.6                     G        R                         Fixed Satellite Service
29.25                  G           30.0                     G        R                         Fixed Satellite Service
18.3                   G           18.8                     G        T                         Fixed Satellite Service
19.7                   G           20.2                     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:
  117 W                                                                                                                                       This orbital location has been selected because,
Longitudinal Tolerance or E/W Station-Keeping:          f. Inclination Excursion or Range of orbital are in which adequate service can be     among other things, it provides high elevation angles
                                                        N/S Station-Keeping         provided (Optional):                                      to all of North America, which is very important for
d. Toward West:                           Degrees                                                                   Degrees       E/W
                                0.05                    Tolerance:
                                                                                                                                              satellite services to large numbers of small and
                                                                                         g. Westernmost:
e. Toward East:                 0.05      Degrees                                                                                             inexpensive consumer earth stations. The high
                                                                 0.05 Degrees            h. Easternmost:                                      elevation minimizes the risk of signal blockage due to
                                                                                                                                              buildings and foliage, and also minimizes the
i. Reason for service are selection (Optional):
                                                                                                                                              atmospheric and rain attenuation.


                                                               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)

NA                 S                                                   CONUS, ALASKA, HAWAII, CANADA, MEXICO


                                                               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)
KAR R            45.5      41.5       0.12       0.12         30 N                          NA                                                 790     16.5          -105            20          1
KAR R            45.5      41.5       0.12       0.12         30 N                          NA                                                 790     16.5          -105            20          1
KAT T            45.5      41.5       0.12       0.12         30 N                          NA                 2           78.9     64.5
KATL T           45.5      41.5       0.12       0.12         30 N                          NA                 2           78.9     64.5


                                                             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)
KAR    R      C               -117                              KARR.gxt
KAR    R      C               -117                              KARL.gxt
KAT    T      C               -117                              KATR.gxt                -118            -118            -118           -118          -118
KATL   T      C               -117                              KATL.gxt                -118            -118            -118           -118          -118


                                                           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)

U001         115000 R        29312.5        L              C           T0001             129.5 U001            KARL        D0001         KATR
U003         115000 R        29437.5        L              C           T0002             129.5 U003            KARL        D0003         KATR
U005         115000   R      28412.5        L              C           T0003             129.5   U005          KARL        D0005         KATR
U007         115000   R      28537.5        L              C           T0004             129.5   U007          KARL        D0007         KATR
U009         115000   R      29562.5        L              C           T0005             129.5   U009          KARL        D0009         KATR
U011         115000   R      29687.5        L              C           T0006             129.5   U011          KARL        D0011         KATR
U013         115000   R      29812.5        L              C           T0007             129.5   U013          KARL        D0013         KATR
U015         115000   R      29937.5        L              C           T0008             129.5   U015          KARL        D0015         KATR
U002         115000   R      29312.5        R              C           T0009             129.5   U002          KARR        D0002         KATL
U004         115000   R      29437.5        R              C           T0010             129.5   U004          KARR        D0004         KATL
U006         115000   R      28412.5        R              C           T0011             129.5   U006          KARR        D0006         KATL
U008         115000   R      28537.5        R              C           T0012             129.5   U008          KARR        D0008         KATL
U010         115000   R      29562.5        R              C           T0013             129.5   U010          KARR        D0010         KATL
U012         115000   R      29687.5        R              C           T0014             129.5   U012          KARR        D0012         KATL
U014         115000   R      29812.5        R              C           T0015             129.5   U014          KARR        D0014         KATL
U016         115000   R      29937.5        R              C           T0016             129.5   U016          KARR        D0016         KATL
D0001        115000   T      18362.5        R              C
D0003        115000   T      18487.5        R              C
D0005        115000   T      18612.5        R              C
D0007        115000   T      18737.5        R              C
D0009        115000   T      19762.5        R              C
D0011        115000   T      19887.5        R              C
D0013        115000   T      20012.5        R              C
D0015        115000   T      20137.5        R              C
D0002        115000   T      18362.5        L              C
D0004        115000   T      18487.5        L              C
D0006        115000   T      18612.5        L              C
D0008        115000   T      18737.5        L              C
D0010        115000   T      19762.5        L              C
D0012        115000   T      19887.5        L              C


D0014   115000 T   20012.5   L   C
D0016   115000 T   20137.5   L   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)

D001           51K2G7W                51.2            4            56          0.691                           8.4            20.6
D002           102KG7W                 102            4           104          0.691                           8.4            20.6
D003           500KG7W               500              4          512           0.691                           8.4            20.6
D004           2M00G7W              2000              4         2048           0.691                           8.4            20.6
D005           6M80G7W              6800              4         6968           0.691                           8.4            20.6
D006           115MG7W            115000              4       117760           0.691                           8.4            20.6


                                                              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)
T0001        T0016      D001                               1790           64 Ka1 LB.doc                             43.9         -15.2        -11.2                                             16.5
T0001        T0016      D002                               1000         125    Ka2 LB.doc                           43.9           -8.2       -12.2                                             16.5
T0001        T0016      D003                                200         575    Ka3 LB.doc                           43.9             -6          -2                                             16.5
T0001        T0016      D004                                 50        2300    Ka4 LB.doc                           43.9              0           4                                             16.5
T0001        T0016      D005                                 16        7187    Ka5 LB.doc                           47.7            1.8         5.8                                             16.5
T0001        T0016      D006                                  1                Ka6 LB.doc                                                                60.5         64.5          -118        17.5


                                                           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:
 530 Echostar Drive
S14b. City:                                S14c. County:                                   S14d. State/Country      S14e. Zip Code:
 Cheyenne                                   Laramie                                          WY                       82007
S14f. Telephone Number:                                    S14g. Call Sign of Control Station (if appropriate):
 (307) 633-5227

Remote Control (TT C) Location(s):
S14a: Street Address:
 801 North American Sky Boulavard
S14b. City:                                S14c. County:                                   S14d. State/Country      S14e. Zip Code:
 Gilbert                                    Maricopa                                         AZ                       85233
S14f. Telephone Number:                                    S14g. Call Sign of Control Station (if appropriate):
 (307) 633-5227


                                                                         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
 2400                                                                      (meters)                         End of Life (0.0 - 1.0)
S15b. Mass of fuel and disposables at launch (kg):
  3400
S15c. Mass of spacecraft and fuel at launch (kg):                  S15f. Length (m):                      S15i. Payload:
  5800                                                              55                                     0.85
S15d. Mass of fuel, in orbit, at beginning of life (kg):           S15g. Width (m):                       S15j. Bus:
  1400                                                              4                                      0.83
S15e. Deployed Area of Solar Array (square meters):                S15h. Height (m):                      S15k. Total:
  110                                                               5                                      0.7055


            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):
                                                14000              14000               14000              14000
            Bus (Watts):                 (b):               (g):                (l):               (q):
                                                1800               925                 1800               925
            Total (Watts):               (c):               (h):                (m):               (r):
                                                15800              14925               15800              14925
            Solar Array (Watts):         (d):               (i):                (n):               (s):
                                                18200              17400               16300              15500
            Depth of Battery             (e)                (j)                 (o)                (t)
            Discharge (%):
                                                75      %                   %          75      %                   %


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: 2004-10-15 12:14:20
Document Modified: 2004-10-15 12:14:20

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