H-2A DEB
Satellite information H-2A DEB
| Spacetrack Directory Name | H-2A DEB |
| Follow H-2A DEB | H-2A DEB Tracker |
| Pass predictions H-2A DEB | Pass predictions H-2A DEB |
| Orbit launches |
2002-02-04 (24 years ago)
|
| Days in orbit | 9028 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 362 km |
| Apogee | 34005 km |
| Orbit slope (inclination) | 28.57° |
| Laps per day | 3 |
| Height H-2A DEB | 22139.8 km |
Additional information H-2A DEB
H-2A DEB, 28243 is space debris in HEO originally from a launch on Mon, 04 Feb 2002 UTC launched from the Tanegashima Space Center (TNSTA). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite H-2A DEB Date of exalting 04.02.2002y. Average height of ISS H-2A DEB hundred 22139.8 km. Average velocity H-2A DEB is 12939.65 km/h. Inclination H-2A DEB satellite 28.43°.TLE
Average velocity H-2A DEB
Average inclination H-2A DEB
Mean right ascension of the ascending node (RAAN) H-2A DEB
Mean argument of perigee H-2A DEB
Mean semi-major axis of the orbit H-2A DEB
Mean orbital eccentricity H-2A DEB
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