USA-246

Summary

USA-246
AEHF 1.jpg
Artist's impression of an AEHF satellite
Mission typeMilitary communications
OperatorUS Air Force
COSPAR ID2013-050A
SATCAT no.39256
Mission duration14 years
Spacecraft properties
BusA2100M
ManufacturerLockheed Martin
Launch mass6,168 kilograms (13,598 lb)
Powerwatts
Start of mission
Launch date18 September 2013, 08:14 UTC
RocketAtlas V 531 (AV-041)
Launch siteCape Canaveral, SLC-41
ContractorULA
Orbital parameters
Reference systemGeocentric
RegimeGeosynchronous
Perigee altitude35,770 kilometers (22,230 mi)
Apogee altitude35,819 kilometers (22,257 mi)
Inclination0.8°
Period23.93 hours
 

USA-246, also known as Advanced Extremely High Frequency 3 or AEHF-3, is a military communications satellite operated by the United States Air Force. It is the third of six spacecraft to be launched as part of the Advanced Extremely High Frequency program, which replaced the earlier Milstar system.[1]

Satellite

The USA-246 spacecraft was constructed by Lockheed Martin, and is based on the A2100 satellite bus. The spacecraft has a mass of 6,168 kilograms (13,598 lb) and a design life of 14 years.[2] It will be used to provide super high frequency and extremely high frequency communications for the armed forces of the United States, as well as those of the United Kingdom, the Netherlands, and Canada.[1]

Launch

Launch of AEHF-3 on an Atlas V

USA-246 was launched by United Launch Alliance, aboard an Atlas V 531 flying from Space Launch Complex 41 at the Cape Canaveral Air Force Station. After a number of weather-related delays, the launch occurred at 08:10 UTC on 18 September 2013,[3] placing the spacecraft in a parking orbit of 178 kilometers by 1,041 kilometers. A second burn placed the satellite into a geosynchronous transfer orbit with a perigee of 225 kilometres (140 mi), an apogee of 50,051 kilometres (31,100 mi), and 20.52° inclination.[4] The satellite was successfully deployed in this orbit 50 minutes after launch.[1]

Orbit

After raising its orbit using its onboard propulsion systems, AEHF-3 was declared operational in late July 2015. It is currently in a 0.8 degree inclination orbit with a perigee of 35,770 kilometers (22,230 mi) and an apogee of 35,819 kilometers (22,257 mi).

See also

References

  1. ^ a b c "AEHF-3 Presskit" (PDF).
  2. ^ Krebs, Gunter. "AEHF 1, 2, 3, 4, 5, 6". Gunter's Space Page. Retrieved 25 March 2021.
  3. ^ Graham, William (17 September 2013). "ULA Atlas V launches with AEHF-3 satellite". NASASpaceFlight.com. Retrieved 27 March 2021.
  4. ^ "JSR News 686".