Attachment Schedule S Tech Data SAT-MOD-20081217-00233

Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20081217-00233 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2008121700233_694537

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:
INTELSAT 702 N

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

c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth:
42 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:
2408 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)
5925 M 6425 M R Fixed Satellite Service
3700 M 4200 M T Fixed Satellite Service
14000 M 14500 M R Fixed Satellite Service
10950 M 11200 M T Fixed Satellite Service
11450 M 11700 M T Fixed Satellite Service
11700 M 11950 M T Fixed Satellite Service
12500 M 12750 M 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:
66 E SPACECRAFT WILL REPLACE INTELSAT 704
Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be
N/S Station-Keeping provided (Optional):
d. Toward West: Degrees E/W
0.05 Degrees Tolerance:
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)

1 S VISIBLE EARTH
2 S EUROPE, AFRICA, MIDDLE EAST, WESTERN ASIA
3 S ASIA, AUSTRALIA
4 S ASIA
5 S SOUTHERN AFRICA
6 S SOUTHEAST ASIA, INDONESIA, AUSTRALIA
7 S EUROPE, AFRICA, MIDDLE EAST, WESTERNA ASIA, SOUTHEAST ASIA, INDONESIA, AUSTRALIA
8 S SOUTHERN AFRICA, ASIA

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)
GAU R 20.3 16.3 N 1 -7 -93.3 14 1
GBU R 20.3 16.3 N 1 -7 -93.2 14 1
WHU R 25.9 19.9 N 2 -1.5 -91.8 14 1
EHU R 23.2 17.2 N 3 -3.5 -91.4 14 1
NWU R 26.8 22.8 N 2 -0.5 -92.9 14 1
NEU R 27.9 23.9 N 4 1 -90.3 14 1
SWU R 27.9 23.9 N 5 0.5 -90.2 14 1
SEUL R 25.6 21.6 N 6 -1.5 -92.4 14 1
X1UL R 22.7 18.7 N 7 -5 -91.1 14 1
X2UL R 24.3 20.3 N 8 -3 -88.8 14 1
CAU R 30.3 26.3 N 1 3 -95.8 14 1
CBU R 30.3 26.3 N 1 3 -96.3 14 1
S1UL R 36.9 32.9 N 01 9.5 -92.6 14 1
S2UL R 34.8 30.8 N 90 1 7 -92.8 14 1
S2AU R 32.9 28.9 N 90 1 5 -92.9 14 1
S3UL R 37.6 33.6 N 01 10 -93.2 14 1
GAD T 20.5 16.5 N 1 29.5
GBD T 20.5 16.5 N 1 30.5
WHD T 27.2 21.2 N 2 38
EHD T 24.5 18.5 N 3 37.5
NWD T 28.7 24.7 N 2 38
NED T 28.6 24.6 N 4 36.5
SWD T 30.8 26.8 N 5 38.5
SEDL T 26.9 22.9 N 6 36.5
CAD T 27.5 23.5 N 1 36.3
CBD T 27.5 23.5 N 1 36.8
S1DL T 36.2 32.2 N 90 1 48.9
S2DL T 34.5 30.5 N 01 49.1
S2AD T 32.7 28.7 N 01 47.2

S3DL T 36.6 32.6 N 90 1 49
CMD R 8.3 5.7 N 1 -28.5 -107.4
TLM T 16.5 13.9 N 1 8.2
TLM T -5.3 -6.3 N 1 0.7
BNC T 10.7 8.1 N 90 1 11.7
BNK1 T 16.7 14.1 N 1 8
BNK2 T 36.2 26.2 N 90 1 11.7
BNK3 T 34.5 24.5 N 0 1 10.3
BNK4 T 32.7 22.7 N 0 1 8.5
BNK5 T 36.6 26.6 N 90 1 12.3

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)
GAU R C 66 gaul.gxt
GBU R C 66 gbul.gxt
WHU R C 66 whul.gxt
EHU R C 66 ehul.gxt
NWU R C 66 nwul.gxt
NEU R C 66 neul.gxt
SWU R C 66 swul.gxt
SEUL R C 66 seul.gxt
X1UL R C 66 x1ul.gxt
X2UL R C 66 x2ul.gxt
CAU R C 66 caul.gxt
CBU R C 66 cbul.gxt
S1UL R C 66 s1ul.gxt
S2UL R C 66 s2ul.gxt
S2AU R C 66 s2au.gxt
S3UL R C 66 s3ul.gxt
GAD T C 66 gadl.gxt -163.8 -163.7 -163.5 -163.4 -163.3
GBD T C 66 gbdl.gxt -162.8 -162.7 -162.5 -162.4 -162.3
WHD T C 66 whdl.gxt -155.3 -155.2 -155 -154.9 -154.8
EHD T C 66 ehdl.gxt -155.8 -155.7 -155.5 -155.4 -155.3
NWD T C 66 nwdl.gxt -155.3 -155.2 -155 -154.9 -154.8
NED T C 66 nedl.gxt -156.8 -156.7 -156.5 -156.4 -156.3
SWD T C 66 swdl.gxt -154.8 -154.7 -154.5 -154.4 -154.3
SEDL T C 66 sedl.gxt -156.8 -156.7 -156.5 -156.4 -156.3
CAD T C 66 cadl.gxt -157 -156.9 -156.7 -156.6 -156.5
CBD T C 66 cbdl.gxt -156.5 -156.4 -156.2 -156.1 -156
S1DL T C 66 s1dl.gxt -150 -147.5 -145 -144 -143.9
S2DL T C 66 s2dl.gxt -150 -147.5 -145 -143.8 -143.7

S2AD T C 66 s2ad.gxt -150 -147.5 -145.8 -145.7 -145.6
S3DL T C 66 s3dl.gxt -150 -147.5 -145 -143.9 -143.8
TLM T C 66 tlmo.gxt -173 -172.9 -172.8 -172.7 -172.6
TLM T C 66 tlmb.gxt -180.5 -180.4 -180.3 -180.2 -180.1
BNC T C 66 bnc.gxt -159.5 -159.4 -159.3 -159.2 -159.1
BNK1 T C 66 bnk1.gxt -163.2 -163.1 -163 -162.9 -162.8
BNK2 T C 66 bnk2.gxt -159.5 -159.4 -159.3 -159.2 -159.1
BNK3 T C 66 bnk3.gxt -160.9 -160.8 -160.7 -160.6 -160.5
BNK4 T C 66 bnk4.gxt -162.7 -162.6 -162.5 -162.4 -162.3
BNK5 T C 66 bnk5.gxt -158.9 -158.8 -158.7 -158.6 -158.5
CMD R C 66 cmd.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)

AUA 36000 R 6280 L C
AUB 36000 R 6320 L C
AUC 36000 R 6360 L C
AUD 41000 R 6402.5 L C
BUA 36000 R 6280 R C
BUB 36000 R 6320 R C
BUC 36000 R 6360 R C
BUD 41000 R 6402.5 R C
CUA 36000 R 6280 L C
CUB 36000 R 6320 L C
CUC 36000 R 6360 L C
CUD 41000 R 6402.5 L C
DUA 36000 R 6280 R C
DUB 36000 R 6320 R C
DUC 36000 R 6360 R C
DUD 41000 R 6402.5 R C
EU1 77000 R 5967.5 L C
EU2 72000 R 6050 L C
EU3 34000 R 6111 L C
EU4 34000 R 6149 L C
EU6 72000 R 6220 L C
EUA 36000 R 6280 L C
FU1 77000 R 5967.5 L C
FU2 72000 R 6050 L C
FU3 34000 R 6111 L C
FU4 34000 R 6149 L C
FU6 72000 R 6220 L C
FUA 36000 R 6280 L C
GU1 77000 R 5967.5 R C
GU2 72000 R 6050 R C

GU3 34000 R 6111 R C
GU4 34000 R 6149 R C
GU6 72000 R 6220 R C
GUA 36000 R 6280 R C
JU1 77000 R 5967.5 R C
JU2 72000 R 6050 R C
JU3 34000 R 6111 R C
JU4 34000 R 6149 R C
JU6 72000 R 6220 R C
JUA 36000 R 6280 R C
HU1 77000 R 5967.5 R C
HU2 72000 R 6050 R C
HU3 34000 R 6111 R C
HU4 34000 R 6149 R C
HU6 72000 R 6220 R C
HUA 36000 R 6280 R C
IU1 77000 R 5967.5 R C
IU2 72000 R 6050 R C
IU3 34000 R 6111 R C
IU4 34000 R 6149 R C
IU6 72000 R 6220 R C
IUA 36000 R 6280 R C
KU1 77000 R 5967.5 R C
KU2 72000 R 6050 R C
KU3 34000 R 6111 R C
KU4 34000 R 6149 R C
KU6 72000 R 6220 R C
KUA 36000 R 6280 R C
LU1 77000 R 5967.5 R C
LU2 72000 R 6050 R C
LU3 34000 R 6111 R C
LU4 34000 R 6149 R C
LU6 72000 R 6220 R C
LUA 36000 R 6280 R C
SU1 77000 R 14042.5 H C
SU2 72000 R 14125 H C
SU3 34000 R 14186 H C
SU4 34000 R 14224 H C
SU6 112000 R 14314 H C

SU7 112000 R 14438 H C
UU1 77000 R 14042.5 V C
UU2 72000 R 14125 V C
UU3 34000 R 14186 V C
UU4 34000 R 14224 V C
UU6 112000 R 14314 V C
UU7 112000 R 14438 V C
YU1 77000 R 14042.5 V C
YU2 72000 R 14125 V C
YU3 34000 R 14186 V C
YU4 34000 R 14224 V C
YU6 112000 R 14314 V C
YU7 112000 R 14438 V C
WU1 77000 R 14042.5 H C
WU2 72000 R 14125 H C
WU3 34000 R 14186 H C
WU4 34000 R 14224 H C
WU6 112000 R 14314 H C
WU7 112000 R 14438 H C
SUC 72000 R 14295 H C
UUC 72000 R 14295 V C
YUC 72000 R 14295 V C
WUC 72000 R 14295 H C
ADA 36000 T 4055 R C
ADB 36000 T 4095 R C
ADC 36000 T 4135 R C
ADD 41000 T 4177.5 R C
CDA 36000 T 4055 R C
CDB 36000 T 4095 R C
CDC 36000 T 4135 R C
CDD 41000 T 4177.5 R C
EDA 36000 T 4055 R C
BDA 36000 T 4055 L C
BDB 36000 T 4095 L C
BDC 36000 T 4135 L C
BDD 41000 T 4177.5 L C
DDA 36000 T 4055 L C
DDB 36000 T 4095 L C
DDC 36000 T 4135 L C

DDD 41000 T 4177.5 L C
FDA 36000 T 4055 R C
ED1 77000 T 3742.5 R C
ED2 72000 T 3825 R C
ED3 34000 T 3886 R C
ED4 34000 T 3924 R C
ED6 72000 T 3995 R C
FD1 77000 T 3742.5 R C
FD2 72000 T 3825 R C
FD3 34000 T 3886 R C
FD4 34000 T 3924 R C
FD6 72000 T 3995 R C
GD1 77000 T 3742.5 L C
GD2 72000 T 3825 L C
GD3 34000 T 3886 L C
GD4 34000 T 3924 L C
GD6 72000 T 3995 L C
GDA 36000 T 4055 L C
JD1 77000 T 3742.5 L C
JD2 72000 T 3825 L C
JD3 34000 T 3886 L C
JD4 34000 T 3924 L C
JD6 72000 T 3995 L C
JDA 36000 T 4055 L C
HD1 77000 T 3742.5 L C
HD2 72000 T 3825 L C
HD3 34000 T 3886 L C
HD4 34000 T 3924 L C
HD6 72000 T 3995 L C
HDA 36000 T 4055 L C
ID1 77000 T 3742.5 L C
ID2 72000 T 3825 L C
ID3 34000 T 3886 L C
ID4 34000 T 3924 L C
ID6 72000 T 3995 L C
IDA 36000 T 4055 L C
S1D1 77000 T 10992.5 V C
S1D2 72000 T 11075 V C
S1D3 34000 T 11136 V C

S1D4 34000 T 11174 V C
S1D6 112000 T 11514 V C
S1D7 112000 T 11638 V C
U1D1 77000 T 10992.5 H C
U1D2 72000 T 11075 H C
U1D3 34000 T 11136 H C
U1D4 34000 T 11174 H C
U1D6 112000 T 11514 H C
U1D7 112000 T 11638 H C
Y1D1 77000 T 10992.5 H C
Y1D2 72000 T 11075 H C
Y1D3 34000 T 11136 H C
Y1D4 34000 T 11174 H C
Y1D6 112000 T 11514 H C
Y1D7 112000 T 11638 H C
W1DA 77000 T 10992.5 V C
W1D2 72000 T 11075 V C
W1D3 34000 T 11136 V C
W1D4 34000 T 11174 V C
W1D6 112000 T 11514 V C
W1D7 112000 T 11638 V C
W1D1 77000 T 10992.5 V C
S2D1 77000 T 12547.5 V C
S2D2 72000 T 12630 V C
S2D3 34000 T 12691 V C
S2D4 34000 T 12729 V C
S2D6 112000 T 11514 V C
S2D7 112000 T 11638 V C
U2D1 77000 T 12547.5 H C
U2D2 72000 T 12630 H C
U2D3 34000 T 12691 H C
U2D4 34000 T 12729 H C
U2D6 112000 T 11514 H C
U2D7 112000 T 11638 H C
Y2D1 77000 T 12547.5 H C
Y2D2 72000 T 12630 H C
Y2D3 34000 T 12691 H C
Y2D4 34000 T 12729 H C
Y2D6 112000 T 11514 H C

Y2D7 112000 T 11638 H C
W2DA 77000 T 12547.5 V C
W2D2 72000 T 12630 V C
W2D3 34000 T 12691 V C
W2D4 34000 T 12729 V C
W2D6 112000 T 11514 V C
W2D7 112000 T 11638 V C
W2D1 77000 T 12547.5 V C
S3D1 77000 T 11747.5 V C
S3D2 72000 T 11830 V C
S3D3 34000 T 11891 V C
S3D4 34000 T 11929 V C
S3D6 112000 T 11514 V C
S3D7 112000 T 11638 V C
U3D1 77000 T 11747.5 H C
U3D2 72000 T 11830 H C
U3D3 34000 T 11891 H C
U3D4 34000 T 11929 H C
U3D6 112000 T 11514 H C
U3D7 112000 T 11638 H C
Y3D1 77000 T 11747.5 H C
Y3D2 72000 T 11830 H C
Y3D3 34000 T 11891 H C
Y3D4 34000 T 11929 H C
Y3D6 112000 T 11514 H C
Y3D7 112000 T 11638 H C
W3DA 77000 T 11747.5 V C
W3D2 72000 T 11830 V C
W3D3 34000 T 11891 V C
W3D4 34000 T 11929 V C
W3D6 112000 T 11514 V C
W3D7 112000 T 11638 V C
W3D1 77000 T 11747.5 V C
S1DC 72000 T 11495 V C
U1DC 72000 T 11495 H C
Y1DC 72000 T 11495 H C
W1DC 72000 T 11495 V C
S2DC 72000 T 11495 V C
U2DC 72000 T 11495 H C

Y2DC 72000 T 11495 H C
W2DC 72000 T 11495 V C
S3DC 72000 T 11495 V C
U3DC 72000 T 11495 H C
Y3DC 72000 T 11495 H C
W3DC 72000 T 11495 V C
CMD2 1000 R 6176.3 L T
TM1 500 T 3947.5 R T
TM2 500 T 3952.5 R T
TM3 500 T 3948 R T
TM4 500 T 3952 R T
BC1 25 T 3950 V T
BK1 25 T 11198 R T
BK2 25 T 11452 R T
BK3 25 T 11701 V T
BK4 25 T 11701 H T
BK5 25 T 11701 H T
BK6 25 T 11701 V T
BK7 25 T 12501 V T
BK8 25 T 12501 H T
BK9 25 T 12501 H T
BK10 25 T 12501 V T
CMD1 1000 R 6173.7 L 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 112MG7W 112000 4 76436 0.5 3.36 15.56
D2 77M0G7W 77000 4 52550 0.5 3.36 15.56
D3 36M0G7W 36000 4 24575 0.5 3.36 15.56
D4 10M3G7W 10300 4 6000 0.5 3.87 16.07
D5 100KG7W 100 4 64 0.5 2.99 15.19
D6 1M45G7W 1450 2 512 0.5 3.4 15.6
D7 400KG7W 400 2 128 0.5 3.4 15.6

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. 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)
A1 30M0F3F 30000 TV/FM 1 PAL 15.6 1.5 10 22.2

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)

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:
3400 INTERNATIONAL DRIVE, N.W.
S14b. City: S14c. County: S14d. State/Country S14e. Zip Code:
WASHINGTON, D.C. DC 20008
S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):
202-944-7701

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:

S16. SPACECRAFT ELECTRICAL CHARACTERISTICS:

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: 2009-02-04 12:57:30
Document Modified: 2009-02-04 12:57:30

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