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USA-298

From Wikipedia, the free encyclopedia
United States Space Force military communications satellite constellation

USA-298
Artist's impression of an AEHF-6 satellite
NamesAEHF-6
Advanced Extremely High Frequency-6
Mission typeMilitary communications
OperatorUnited States Space Force
COSPAR ID2020-022BEdit this at Wikidata
SATCATno.45465
Websitehttps://www.spaceforce.mil/
Mission duration14 years (planned)
5 years and 5 days(in progress)
Spacecraft properties
SpacecraftAEHF-5
BusA2100M
ManufacturerLockheed Martin Space
Launch mass6,168 kg (13,598 lb)
Start of mission
Launch date26 March 2020, 20:18:00UTC
RocketAtlas V 551 (AV-086)
Launch siteCape Canaveral,SLC-41
ContractorUnited Launch Alliance
Orbital parameters
Reference systemGeocentric orbit
RegimeGeosynchronous orbit
← AEHF-5

USA-298, also known asAdvanced Extremely High Frequency 6 orAEHF-6, is a militarycommunications satellite operated by theUnited States Space Force (USSF). It is the sixth of six satellite to be launched as part of theAdvanced Extremely High Frequency program, which replaced the earlierMilstar system.[1]

Satellite description

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The USA-298 satellite was constructed byLockheed Martin Space, and is based on theA2100satellite 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 providesuper high frequency (SHF) andextremely high frequency (EHF) communications for theUnited States Armed Forces, as well as those of the United Kingdom, the Netherlands, Canada, and Australia.[2]

Launch

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USA-298 was launched byUnited Launch Alliance, aboard anAtlas V 551 flying fromSLC-41 at theCape Canaveral Air Force Station (CCAFS). The launch occurred at 20:18:00UTC on 26 March 2020,[3] placing the satellite into ageostationary transfer orbit (GTO) with aperigee of 12,543 km (7,794 mi), anapogee of 30,672 km (19,059 mi), and 9.95°inclination.[4] The satellite was successfully deployed in this orbit about five and a half hours after launch.

TDO-2 satellite

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Alongside AEHF-6, theU.S. Air ForceSpace and Missile Systems Center launched an experimental 12Ucubesat known as TDO-2 (Technology Demonstration Orbiter). The satellite was deployed, after 30 minutes in the flight,[5] prior to AEHF-6, from a dispenser on the aft of theCentaur upper stage into an orbit with a perigee of 200 km (120 mi) and an apogee of 35,459 km (22,033 mi).[6]

See also

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References

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  1. ^"Atlas V - AEHF-6". United Launch Alliance. 6 April 2020. Retrieved18 May 2021.
  2. ^ab"AEHF 1, 2, 3, 4, 5, 6". Gunter's Space Page. 4 November 2020. Retrieved18 May 2021.
  3. ^"ULA launches final AEHF satellite atop Atlas V". SpaceFlight Insider. 26 March 2020. Retrieved18 May 2021.
  4. ^"AEHF-6 Mission Overview". United Launch Alliance. Retrieved18 May 2021.
  5. ^"Final AEHF satellite mated to Atlas 5 launcher at Cape Canaveral". Spaceflight Now. 12 March 2020. Retrieved18 May 2021.
  6. ^"TDO 1, 2, 3, 4". Gunter's Space Page. 16 May 2021. Retrieved18 May 2021.
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Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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