Attachment Schedule S Tech Data SAT-LOI-20041228-00229

Attachment Schedule S Tech Data

This document pretains to SAT-LOI-20041228-00229 for Letter of Intent on a Satellite Space Stations filing.

IBFS_SATLOI2004122800229_413823

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:
SPECTRUM IA 2/1/2010 N

b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis:
6/1/2006 12 Years 0

c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth:
6/1/2009 202 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:
10/1/2009 12/1/2009 4848 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)
12.2 G 12.7 G T Broadcasting Satellite Service - Video
12.2 G 12.7 G T Broadcasting Satellite Service - Data
12.2 G 12.7 G T Broadcasting Satellite Service - Sound
12.2 G 12.7 G T TT & C
17.3 G 17.8 G R Broadcasting Satellite Service - Video
17.3 G 17.8 G R Broadcasting Satellite Service - Data
17.3 G 17.8 G R Broadcasting Satellite Service - Sound
17.3 G 17.8 G R TT & C

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:
114.5 W This is an orbital slot with full CONUS coverage and is
Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be compatible with the Region 2 BSS Plan.
N/S Station-Keeping provided (Optional):
d. Toward West: Degrees E/W
0.05 Degrees Tolerance:
g. Westernmost: 1 W
e. Toward East: 0.05 Degrees 0.05 Degrees h. Easternmost: 1 E
i. Reason for service are selection (Optional):
Compatibility with Region 2 BSS plan APS30, APS30A

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)

CONUS S 1-48 coaxial uplink/downlink spot beams, 0.7 deg beamwidth
ALASKA S Beam 49 coaxial uplink/downlink spot beams, 6.0 deg beamwidth
HAWAII S Beam 50 coaxial uplink/downlink spot beams, 0.7 deg beamwidth
ANTILLES S Beam 51 coaxial uplink/downlink spot beams, 0.7 deg beamwidth
ANTILLES S Beam 52 coaxial uplink/downlink spot beams, 0.7 deg beamwidth

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)
1 R 49.4 45.4 0.05 0 30 N CONUS 1.5 3.09 65.3 646 17.3 -87.9 10 1
2 R 49.4 45.4 0.05 0 30 N CONUS 1.5 4.1 55.5 646 17.3 -87.9 10 1
3 R 49.4 45.4 0.05 0 30 N CONUS 1.5 1.2 65.6 646 17.3 -87.9 10 1
4 R 49.4 45.4 0.05 0 30 N CONUS 1.5 4.3 55.7 646 17.3 -87.9 10 1
5 R 49.4 45.4 0.05 0 30 N CONUS 1.5 4.4 55.8 646 17.3 -87.9 10 1
6 R 49.4 45.4 0.05 0 30 N CONUS 1.5 4.5 55.9 646 17.3 -87.8 10 1
7 R 49.4 45.4 0.05 0 30 N CONUS 1.5 4.6 56 646 17.3 -87.8 10 1
8 R 49.4 45.4 0.05 0 30 N CONUS 1.5 4.6 56 646 17.3 -87.8 10 1
9 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.7 57 646 17.3 -83.1 10 1
10 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.7 57 646 17.3 -83.1 10 1
11 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.8 57 646 17.3 -83.5 10 1
12 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.8 57 646 17.3 -83.9 10 1
13 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.9 57.1 646 17.3 -84.1 10 1
14 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.9 57.1 646 17.3 -84.1 10 1
15 R 49.4 45.4 0.05 0 30 N CONUS 1.5 6 57.2 646 17.3 -84.3 10 1
16 R 49.4 45.4 0.05 0 30 N CONUS 1.5 6 57.2 646 17.3 -84.3 10 1
17 R 49.4 45.4 0.05 0 30 N CONUS 1.5 6 57.2 646 17.3 -84.3 10 1
18 R 49.4 45.4 0.05 0 30 N CONUS 1.5 6 57.2 646 17.3 -84.3 10 1
19 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.2 56.6 646 17.3 -88.9 10 1
20 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.3 56.6 646 17.3 -88.9 10 1
21 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.5 56.8 646 17.3 -88.9 10 1
22 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.5 56.8 646 17.3 -88.9 10 1
23 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.7 57 646 17.3 -88.9 10 1
24 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.8 57 646 17.3 -88.9 10 1
25 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.9 57.1 646 17.3 -87.1 10 1
26 R 49.4 45.4 0.05 0 30 N CONUS 1.5 6 57.2 646 17.3 -85.3 10 1
27 R 49.4 45.4 0.05 0 30 N CONUS 1.5 6 57.2 646 17.3 -83.4 10 1
28 R 49.4 45.4 0.05 0 30 N CONUS 1.5 6 57.2 646 17.3 -83.4 10 1
29 R 49.4 45.4 0.05 0 30 N CONUS 1.5 6 57.2 646 17.3 -83.4 10 1

30 R 49.4 45.4 0.05 0 30 N CONUS 1.5 2.9 54 646 17.3 -89.6 10 1
31 R 49.4 45.4 0.05 0 30 N CONUS 1.5 2.9 54 646 17.3 -89.6 10 1
32 R 49.4 45.4 0.05 0 30 N CONUS 1.5 3.3 54.6 646 17.3 -89.6 10 1
33 R 49.4 45.4 0.05 0 30 N CONUS 1.5 4.3 55.7 646 17.3 -87.9 10 1
34 R 49.4 45.4 0.05 0 30 N CONUS 1.5 4.3 55.7 646 17.3 -86.2 10 1
35 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.5 56.8 646 17.3 -84.5 10 1
36 R 49.4 45.4 0.05 0 30 N CONUS 1.5 6.3 57.4 646 17.3 -84.5 10 1
37 R 49.4 45.4 0.05 0 30 N CONUS 1.5 7.1 57.9 646 17.3 -84.5 10 1
38 R 49.4 45.4 0.05 0 30 N CONUS 1.5 7.9 58.4 646 17.3 -84.5 10 1
39 R 49.4 45.4 0.05 0 30 N CONUS 1.5 8.8 58.8 646 17.3 -84.5 10 1
40 R 49.4 45.4 0.05 0 30 N CONUS 1.5 2.8 53.9 646 17.3 -89.5 10 1
41 R 49.4 45.4 0.05 0 30 N CONUS 1.5 2.8 53.9 646 17.3 -87 10 1
42 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5 56.4 646 17.3 -84.4 10 1
43 R 49.4 45.4 0.05 0 30 N CONUS 1.5 7.2 58 646 17.3 -81.8 10 1
44 R 49.4 45.4 0.05 0 30 N CONUS 1.5 7.2 58 646 17.3 -81.8 10 1
45 R 49.4 45.4 0.05 0 30 N CONUS 1.5 7.2 58 646 17.3 -81.8 10 1
46 R 49.4 45.4 0.05 0 30 N CONUS 1.5 7.2 58 646 17.3 -81.8 10 1
47 R 49.4 45.4 0.05 0 30 N CONUS 1.5 5.5 56.8 646 17.3 -84.5 10 1
48 R 49.4 45.4 0.05 0 30 N CONUS 1.5 15.8 61.4 646 17.3 -73.6 10 1
49 R 35.4 31.4 0.05 0 30 N ALASKA 1.5 17.9 55.3 646 17.3 -73.9 10 1
50 R 49.4 45.4 0.05 0 30 N HAWAII 1.5 15.8 61.4 646 17.3 -73.6 10 1
51 R 49.4 45.4 0.05 0 30 N ANTILLES 1.5 15.8 61.4 646 17.3 -73.6 10 1
NOT T
NOT R
52 R 49.4 45.4 0.05 0 30 N ANTILLES 1.5 15.8 61.4 646 17.3 -73.6 10 1
T

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)
18 T C -114.5 -136 -133.1 -127 -122.4 -122.7
49 T C -114.5 -125 -125 -125 -125 -125

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)

1-A 24000 R 17388.58 L C T-1A 158.4 1-A 1-A'
2-A 24000 R 17445.22 L C T-2A 158.4 2-A 2-A'
3-A 24000 R 17571.86 L C T-3A 158.4 3-A 3-A'
4-A 24000 R 17688.50 L C T-4A 158.4 4-A 4-A'
1-B 24000 R 17367.74 L C T-1B 158.4 1-B 1-B'
2-B 24000 R 17484.58 L C T-2B 158.4 2-B 2-B'
3-B 24000 R 17601.02 L C T-3B 158.4 3-B 3-B'
4-B 24000 R 17717.66 L C T-4B 158.4 4-B 4-B'
1-C 24000 R 17396.90 L C T-1C 158.4 1-C 1-C'
2-C 24000 R 17513.54 L C T-2C 158.4 2-C 2-C'
3-C 24000 R 17630.18 L C T-3C 158.4 3-C 3-C'
4-C 24000 R 17746.82 L C T-4C 158.4 4-C 4-C'
1-D 24000 R 17426.06 L C T-1D 158.4 1-D 1-D'
2-D 24000 R 17542.70 L C T-2D 158.4 2-D 2-D'
3-D 24000 R 17659.34 L C T-3D 158.4 3-D 3-D'
4-D 24000 R 17775.98 L C T-4D 158.4 4-D 4-D'
1-A' 24000 T 12238.58 R C T-5 5 NOTE
2-A' 24000 T 12335.22 R C T-6 6 NOTE
3-A' 24000 T 12471.86 R C T-7 7 NOTE
4-A' 24000 T 12558.50 R C T-8 8 NOTE
1-B' 24000 T 12267.74 R C
2-B' 24000 T 12384.38 R C
3-B' 24000 T 12501.02 R C
4-B' 24000 T 12617.66 R C
1-C' 24000 T 12296.90 R C
2-C' 24000 T 12413.54 R C
3-C' 24000 T 12530.18 R C
4-C' 24000 T 12646.82 R C
1-D' 24000 T 12326.06 R C
2-D' 24000 T 12442.70 R C

3-D' 24000 T 12559.34 R C
4-D' 24000 T 12675.98 R C
5 1000 R 17305 L T
6 1000 T 12201 L T
7 1000 T 12203 L T
8 1000 T 12201.5 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)

AA 24M0G1W 24000 4 27600 0.75 7 15.2
BB 1M00G2D 1000 2 2.4 21.3

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)
T-1A T-4D AA 1 Table 3.doc 49.4 4.5 12 54 61.4 -118.9 13.1
T-6 BB 1 Table 4.doc 19 0 0 16 19 -206.3 37
T-7 BB 1 Table 4.doc 19 0 0 16 19 -206.3 37

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:

S14b. City: S14c. County: S14d. State/Country S14e. Zip Code:
Curacao
S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):

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
2221 (meters) End of Life (0.0 - 1.0)
S15b. Mass of fuel and disposables at launch (kg):
3920
S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload:
6533 24 0.9
S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus:
392 3 0.9
S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total:
61.8 4 0.81

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):
4508 4508 4508 4508
Bus (Watts): (b): (g): (l): (q):
1032 1002 1032 1002
Total (Watts): (c): (h): (m): (r):
5540 5510 5540 5510
Solar Array (Watts): (d): (i): (n): (s):
7293 6644 6081 5540
Depth of Battery (e) (j) (o) (t)
Discharge (%):
75 % 0 % 75 % 0 %

S17. CERTIFICATIONS:
a. Are the power flux density limits of § 25.208 met?: YES NO X 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 X 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: 2005-01-18 09:37:23
Document Modified: 2005-01-18 09:37:23

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