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The mobile telecommunication satellite will be
positioned at 44° E. The satellite is owned, and will be operated
by Thuraya Satellite Telecommunications Co. Ltd., Abu Dhabi,
United Arab Emirates.
The
5250 kg (11,576 lbm) satellite is derived from the BSS 702
(formerly the HS 702) model. The US$960 million contract with
Thuraya Satellite Telecommunications Company was signed by Hughes
in 1997. It included the manufacture of two high-power BSS GEM
(formerly HS GEM) satellites, launch of the first spacecraft,
insurance, ground facilities, and user handsets. The second
satellite is a ground spare, with an option for a third. The
Thuraya ground segment includes terrestrial gateways plus a
collocated network operations center and satellite control
facility in the United Arab Emirates.
Thuraya 1 will
transmit and receive calls through a single 12.25-meter aperture
reflector. The reflector transmits and receives signals for an
L-band feed array. The reflector weighs 78 kg (170 lbm), and
compresses into a compact package 1.3 m (50 in) diameter by 3.8 m
(150 in) for launch. Solar power is derived from two wings of four
panels each with dual-junction gallium arsenide solar cells. In
orbit, the satellite measures 34.5 m (113 ft) in length and 17 m
(55.7 ft) in width, and will weigh 3200 kg (7056 lbm).

| Thuraya
1
|
|
Spacecraft
|
| Int'l Designation |
2000
066A
|
launched
|
| Owner / Sponsor |
Thuraya
Satellite Telecommunications Co. Ltd.
|
| Mission |
Telecommunications
|
| Manufacturer / Model |
Boeing
Satellite Systems
|
BSS-GEM (based
on BSS-702)
|
| Launch Mass |
5250
kg (11,576 lbm)
|
| Dimensions, stowed |
7.6
m (25 ft) x 3.75 m x 3.75 m (12.3 ft)
|
| Mission Orbit |
GSO
|
44°E
|
| Design Life |
12
years
|
| Power (EOL) |
11
kW
|
|
Launch
|
| Launch Vehicle
Model |
Zenit
3SL/DMSL |
| Date / Time (UTC) |
2000
October 21
|
00:52
|
|
Financial
|
| Satellite cost |
Total
Project cost US$960 million
|
| Web Links |
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