THEMIS A
Satellite information THEMIS A
| Spacetrack Directory Name | THEMIS A |
| Alternative name | TIME HISTORY OF EVENTS AND MACROSCALE INTERACTIONS DURING SUBSTORMS 1 |
| Follow THEMIS A | THEMIS A Tracker |
| Pass predictions THEMIS A | Pass predictions THEMIS A |
| Orbit launches |
2007-02-17 (19 years ago)
|
| Days in orbit | 7090 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Categories | |
| Perigee | 1030 km |
| Apogee | 78328 km |
| Orbit slope (inclination) | 8.67° |
| Laps per day | 1 |
| Orbit | Elliptical |
| Height THEMIS A | 55979.92 km |
Additional information THEMIS A
THEMIS A, 30580 is a payload satellite owned by GSFC (US) in HEO that was launched on Sat, 17 Feb 2007 UTC via a DELTA 7925-10C launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite THEMIS A Date of exalting 17.02.2007y. Average height of ISS THEMIS A hundred 55979.92 km. Average velocity THEMIS A is 8340.18 km/h. Inclination THEMIS A satellite 5.86°.TLE
Average orbit height THEMIS A
Average velocity THEMIS A
Average inclination THEMIS A
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