Attachment Schedule S Tech Data SAT-MOD-20040812-00159

Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20040812-00159 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2004081200159_389245

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:
SATCOM-C3 10/16/1992 N

b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis:
4.3 Years 0

c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth:
24 0 MHz

d. Estimated Launch Date: h. Total Transponder Bandwidth (no. transponders x Bandwidth) l. Orbit Type: Mark all boxes that apply:
8/31/1992 864 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)
3700 M 4200 M T Direct to Home in the Fixed Fixed Satellite Service
3700 M 4200 M T Fixed Satellite Service
5925 M 6425 M R Direct to Home in the Fixed Fixed Satellite Service
5925 M 6425 M 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:
79 W SES Americom proposes to relocate C-3 to 79 W.L. in
Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be order to provide follow-on C-band capacity at that
N/S Station-Keeping provided (Optional): location.
d. Toward West: Degrees Degrees E/W
0.05 Tolerance:
g. Westernmost: W
e. Toward East: 0.05 Degrees
10 Degrees h. Easternmost: W
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)

CNA E -7 dB gain contour of beams CUH and CUV for the uplink; -8 dB gain contour of beams CDH and CDV for the do

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)
CDH T 30 22 0.12 0 30 Y 0 CNA 1 13.6 41.4
CDV T 30.1 22.1 0.12 0 32 Y 90 CNA 1 14 41.6
CUH R 30.1 23.1 0.12 0 32 Y 0 CNA 525 2.9 -97.2 18 2
CUV R 31.2 24.2 0.12 0 36 Y 90 CNA 615 3.3 -98.2 18 2

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)
CDH T C -79 C3 CDH C11.gxt -152 -150 -150 -149 -148
CDV T C -79 C3 CDV Ch12.gxt -152 -150 -150 -149 -148
CUH R C -79 C3 CUH Ch12.gxt
CUV R C -79 C3 CUV C11.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)

CD001 36000 T 3720 H C C0001 112 CU001 CUV CD001 CDH
CD003 36000 T 3760 H C C0003 112 CU003 CUV CD003 CDH
CD005 36000 T 3800 H C C0005 112 CU005 CUV CD005 CDH
CD007 36000 T 3840 H C C0007 112 CU007 CUV CD007 CDH
CD009 36000 T 3880 H C C0009 112 CU009 CUV CD009 CDH
CD011 36000 T 3920 H C C0011 112 CU011 CUV CD011 CDH
CD013 36000 T 3960 H C C0013 112 CU013 CUV CD013 CDH
CD015 36000 T 4000 H C C0015 112 CU015 CUV CD015 CDH
CD017 36000 T 4040 H C C0017 112 CU017 CUV CD017 CDH
CD019 36000 T 4080 H C C0019 112 CU019 CUV CD019 CDH
CD021 36000 T 4120 H C C0021 112 CU021 CUV CD021 CDH
CD023 36000 T 4160 H C C0023 112 CU023 CUV CD023 CDH
CD002 36000 T 3740 V C C0002 112 CU002 CUH CD002 CDV
CD004 36000 T 3780 V C C0004 112 CU004 CUH CD004 CDV
CD006 36000 T 3820 V C C0006 112 CU006 CUH CD006 CDV
CD008 36000 T 3860 V C C0008 112 CU008 CUH CD008 CDV
CD010 36000 T 3900 V C C0010 112 CU010 CUH CD010 CDV
CD012 36000 T 3940 V C C0012 112 CU012 CUH CD012 CDV
CD014 36000 T 3980 V C C0014 112 CU014 CUH CD014 CDV
CD016 36000 T 4020 V C C0016 112 CU016 CUH CD016 CDV
CD018 36000 T 4060 V C C0018 112 CU018 CUH CD018 CDV
CD020 36000 T 4100 V C C0020 112 CU020 CUH CD020 CDV
CD022 36000 T 4140 V C C0022 112 CU022 CUH CD022 CDV
CD024 36000 T 4180 V C C0024 112 CU024 CUH CD024 CDV
CU001 36000 R 5945 V C
CU003 36000 R 5985 V C
CU005 36000 R 6025 V C
CU007 36000 R 6065 V C
CU009 36000 R 6105 V C
CU011 36000 R 6145 V C

CU013 36000 R 6185 V C
CU015 36000 R 6225 V C
CU017 36000 R 6265 V C
CU019 36000 R 6305 V C
CU021 36000 R 6345 V C
CU023 36000 R 6385 V C
CU002 36000 R 5965 H C
CU004 36000 R 6005 H C
CU006 36000 R 6045 H C
CU008 36000 R 6085 H C
CU010 36000 R 6125 H C
CU012 36000 R 6165 H C
CU014 36000 R 6205 H C
CU016 36000 R 6245 H C
CU018 36000 R 6285 H C
CU020 36000 R 6325 H C
CU022 36000 R 6365 H C
CU024 36000 R 6405 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)

A 36M0G7W 36000 4 40000 0.691 6.8 19
B 6M95G1W 6950 4 8000 0.691 6.8 19
C 36M0G7W 36000 8 60000 0.614 9.9 22.1
D 100KG1W 100 4 56 0.691 6.8 19
E 1M35G7W 1350 4 1544 0.691 6.8 19

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)
F 36M0F3F 36000 TV/FM 1 NTSC 12.8 1.29 12 26

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)
C0001 C0024 A 1 6 53.8 14 32 31.1 41.6 -159.3 22.3
C0001 C0024 B 5 6950 6 53.8 -1.5 16.5 22.1 34.5 -159.5 23.7
C0001 C0024 C 1 8 53.8 14 32 32.3 41.6 -159.8 29.8
C0001 C0024 D 360 100 10 47.8 -14.5 3.5 3.8 16 -156.3 22.3
C0001 C0024 E 26 1350 10 47.8 0.7 18.7 17.6 27.3 -159.4 22.3
C0001 C0024 F 1 12 3300 53.2 14.6 32.6 35.3 41.6 -149.9 23.7

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:
Woodbine TT&C
S14b. City: S14c. County: S14d. State/Country S14e. Zip Code:
Mt. Airy MD 21771
S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):
410-549-4300 E7169

Remote Control (TT C) Location(s):
S14a: Street Address:
Vernon Valley Spacecraft Ops
S14b. City: S14c. County: S14d. State/Country S14e. Zip Code:
Sussex NJ 07461
S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):
973-823-6000 WB81

Remote Control (TT C) Location(s):
S14a: Street Address:
Grand Junction
S14b. City: S14c. County: S14d. State/Country S14e. Zip Code:
Grand Junction CO 81505
S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):
970-241-8300 E890537

Remote Control (TT C) Location(s):
S14a: Street Address:
SES Americom
S14b. City: S14c. County: S14d. State/Country S14e. Zip Code:
Somis CA 93066
S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):
805-386-4195 E940156

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
624 (meters) End of Life (0.0 - 1.0)
S15b. Mass of fuel and disposables at launch (kg):
779
S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload:
1402 15.24 0.71
S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus:
181 1.32 0.77
S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total:
14.72 3.76 0.55

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):
1023 1023 1023 1023
Bus (Watts): (b): (g): (l): (q):
294 275 294 275
Total (Watts): (c): (h): (m): (r):
1317 1298 1317 1298
Solar Array (Watts): (d): (i): (n): (s):
1974 1974 1365 1365
Depth of Battery (e) (j) (o) (t)
Discharge (%):
60 % % 60 % %

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: 2004-08-13 18:13:19
Document Modified: 2004-08-13 18:13:19

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