GEOTAIL
Satellite information GEOTAIL
| Spacetrack Directory Name | GEOTAIL |
| Follow GEOTAIL | GEOTAIL Tracker |
| Pass predictions GEOTAIL | Pass predictions GEOTAIL |
| Orbit launches |
1992-07-24 (34 years ago)
|
| Days in orbit | 12464 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 57184 km |
| Apogee | 183717 km |
| Orbit slope (inclination) | 45.51° |
| Laps per day | 0 |
| Orbit | Elliptical (Deep Highly Eccentric) |
| Height GEOTAIL | 140048.41 km |
Additional information GEOTAIL
GEOTAIL, 22049 is a payload satellite owned by ISAS (JP) in HEO that was launched on Fri, 24 Jul 1992 UTC via a DELTA 6925 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 GEOTAIL Date of exalting 24.07.1992y. Average height of ISS GEOTAIL hundred 140048.41 km. Average velocity GEOTAIL is 5858.51 km/h. Inclination GEOTAIL satellite 45.48°.TLE
Average velocity GEOTAIL
Average inclination GEOTAIL
Mean right ascension of the ascending node (RAAN) GEOTAIL
Mean argument of perigee GEOTAIL
Mean semi-major axis of the orbit GEOTAIL
Mean orbital eccentricity GEOTAIL
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