Names | WGS-5 WGS SV-5 Wideband Global SATCOM-5 |
---|---|
Mission type | Military communications |
Operator | United States Air Force / United States Space Force |
COSPAR ID | 2013-024A |
SATCAT no. | 39168 |
Website | https://www.spaceforce.mil/ |
Mission duration | 14 years (planned) 11 years, 4 months and 9 days (in progress) |
Spacecraft properties | |
Spacecraft | WGS-5 |
Spacecraft type | WGS Block II |
Bus | BSS-702HP |
Manufacturer | Boeing Satellite Systems |
Launch mass | 5,987 kg (13,199 lb) [1] |
Dry mass | 3,000 kg (6,600 lb) |
Power | 11 kW |
Start of mission | |
Launch date | 25 May 2013, 00:27 UTC |
Rocket | Delta IV M+ (5,4) (s/n D362) |
Launch site | Cape Canaveral, SLC-37B |
Contractor | United Launch Alliance |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Geostationary orbit |
Longitude | 52.5° West (Contiguous United States) |
Transponders | |
Band | X-band and Ka-band |
Frequency | 7.2/8.4 GHz (X-band) 30/20 GHz (Ka-band) |
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USA-243, also known as WGS-5, is a United States military communications satellite. It was the fifth satellite to be launched as part of the Wideband Global SATCOM program[2] and the second Block II satellite.[3]