THEMIS E
Satellite information THEMIS E
| Spacetrack Directory Name | THEMIS E |
| Alternative name | TIME HISTORY OF EVENTS AND MACROSCALE INTERACTIONS DURING SUBSTORMS 5 |
| Follow THEMIS E | THEMIS E Tracker |
| Pass predictions THEMIS E | Pass predictions THEMIS E |
| Orbit launches |
2007-02-17 (19 years ago)
|
| Days in orbit | 7136 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Categories | |
| Perigee | 1233 km |
| Apogee | 78121 km |
| Orbit slope (inclination) | 6.98° |
| Laps per day | 1 |
| Orbit | Elliptical |
| Height THEMIS E | 55895.94 km |
Additional information THEMIS E
THEMIS E, 30798 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 E Date of exalting 17.02.2007y. Average height of ISS THEMIS E hundred 55895.94 km. Average velocity THEMIS E is 8348.86 km/h. Inclination THEMIS E satellite 4.12°.TLE
Average velocity THEMIS E
Average inclination THEMIS E
Mean right ascension of the ascending node (RAAN) THEMIS E
Mean argument of perigee THEMIS E
Mean semi-major axis of the orbit THEMIS E
Mean orbital eccentricity THEMIS E
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