Jump to content

USA-288

From Wikipedia, the free encyclopedia
(Redirected from AEHF-4)

USA-288
Artist's impression of an AEHF-4 satellite
NamesAEHF-4
Advanced Extremely High Frequency-4
Mission typeMilitary communications
OperatorUnited States Air Force / United States Space Force
COSPAR ID2018-079A Edit this at Wikidata
SATCAT no.43651
Websitehttps://www.spaceforce.mil/
Mission duration14 years (planned)
6 years and 10 days (in progress)
Spacecraft properties
SpacecraftAEHF-4
BusA2100M
ManufacturerLockheed Martin Space
Launch mass6,168 kg (13,598 lb)
Start of mission
Launch date17 October 2018, 04:15 UTC
RocketAtlas V 551 (AV-079)
Launch siteCape Canaveral, SLC-41
ContractorUnited Launch Alliance
Orbital parameters
Reference systemGeocentric orbit
RegimeGeosynchronous orbit
← AEHF-3
AEHF-5 →

USA-288, also known as Advanced Extremely High Frequency 4 or AEHF-4, is a military communications satellite operated by the United States Air Force. It is the fourth of six satellite to be launched as part of the Advanced Extremely High Frequency program, which replaced the earlier Milstar system.[1]

Satellite description

[edit]

The USA-288 satellite was constructed by Lockheed Martin Space, and is based on the A2100 satellite bus. The satellite has a mass of 6,168 kg (13,598 lb) and a design life of 14 years.[2] It will be used to provide super high frequency (SHF) and extremely high frequency (EHF) communications for the United States Armed Forces, as well as those of the United Kingdom, the Netherlands, and Canada.[2]

Launch

[edit]
Launch of AEHF-4 on an Atlas V

USA-288 was launched by United Launch Alliance, aboard an Atlas V 551 flying from SLC-41 at the Cape Canaveral Air Force Station (CCAFS). The launch occurred at 04:15 UTC on 17 October 2018,[3] placing the satellite in a parking orbit of 176 kilometers by 485 kilometers. A second burn placed the satellite into a geostationary transfer orbit (GTO) with a perigee of 202 km (126 mi), an apogee of 22,578 km (14,029 mi), and 25.9° inclination.[4] A third and final burn, designed to minimize the amount of orbit raising required by the satellite, placed AEHF-4 in a 12.8° inclination orbit with a perigee of 8,914 kilometers and an apogee of 35,300 kilometers.[4] The satellite was successfully deployed in this orbit about three and a half hours after launch.[1]

See also

[edit]

References

[edit]
  1. ^ a b "AEHF-4 Mission Overview" (PDF). United Launch Alliance. Retrieved 18 May 2021.
  2. ^ a b "AEHF 1, 2, 3, 4, 5, 6". Gunter's Space Page. 4 November 2020. Retrieved 17 May 2021.
  3. ^ "Atlas V 551 launches AEHF-4 for the US Air Force". NASASpaceFlight.com. 16 October 2018. Retrieved 18 May 2021.
  4. ^ a b "JSR No.755". Jonathan's Space Report. 18 October 2018. Retrieved 18 May 2021.