ETS 6 DEB
Satellite information ETS 6 DEB
| Spacetrack Directory Name | ETS 6 DEB |
| Follow ETS 6 DEB | ETS 6 DEB Tracker |
| Pass predictions ETS 6 DEB | Pass predictions ETS 6 DEB |
| Orbit launches |
1994-08-28 (32 years ago)
|
| Days in orbit | 11695 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 7835 km |
| Apogee | 38649 km |
| Orbit slope (inclination) | 12.12° |
| Laps per day | 2 |
| Height ETS 6 DEB | 27233.58 km |
Additional information ETS 6 DEB
ETS 6 DEB, 23248 is space debris in HEO originally from a launch on Sun, 28 Aug 1994 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 ETS 6 DEB Date of exalting 28.08.1994y. Average height of ISS ETS 6 DEB hundred 27233.58 km. Average velocity ETS 6 DEB is 12257.9 km/h. Inclination ETS 6 DEB satellite 12.1°.TLE
Average velocity ETS 6 DEB
Average inclination ETS 6 DEB
Mean right ascension of the ascending node (RAAN) ETS 6 DEB
Mean argument of perigee ETS 6 DEB
Mean semi-major axis of the orbit ETS 6 DEB
Mean orbital eccentricity ETS 6 DEB
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