ERS 2 DEB
Satellite information ERS 2 DEB
| Spacetrack Directory Name | ERS 2 DEB |
| Follow ERS 2 DEB | ERS 2 DEB Tracker |
| Pass predictions ERS 2 DEB | Pass predictions ERS 2 DEB |
| Orbit launches |
1995-04-21 (31 years ago)
|
| Days in orbit | 11469 |
| Country/organisation of origin | European Space Agency (ESA) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 763 km |
| Apogee | 772 km |
| Orbit slope (inclination) | 98.62° |
| Laps per day | 14 |
| Height ERS 2 DEB | 739.53 km |
Additional information ERS 2 DEB
ERS 2 DEB, 35391 is space debris in SSO originally from a launch on Fri, 21 Apr 1995 UTC launched from the French Guiana (FRGUI). 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 ERS 2 DEB Date of exalting 21.04.1995y. Average height of ISS ERS 2 DEB hundred 739.53 km. Average velocity ERS 2 DEB is 26951.92 km/h. Inclination ERS 2 DEB satellite 98.62°.TLE
Average velocity ERS 2 DEB
Average inclination ERS 2 DEB
Mean right ascension of the ascending node (RAAN) ERS 2 DEB
Mean argument of perigee ERS 2 DEB
Mean semi-major axis of the orbit ERS 2 DEB
Mean orbital eccentricity ERS 2 DEB
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