ELEKTRON 1 DEB *
Satellite information ELEKTRON 1 DEB * - ELEKTRON 1 DEB
| Spacetrack Directory Name | ELEKTRON 1 DEB * |
| Alternative name | ELEKTRON 1 DEB |
| Follow ELEKTRON 1 DEB * | ELEKTRON 1 DEB * Tracker |
| Pass predictions ELEKTRON 1 DEB * | Pass predictions ELEKTRON 1 DEB * |
| Orbit launches |
1964-01-30 (62 years ago)
|
| Days in orbit | 22920 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 707 km |
| Apogee | 4900 km |
| Orbit slope (inclination) | 58.96° |
| Laps per day | 10 |
| Height ELEKTRON 1 DEB * | 2942.24 km |
Additional information ELEKTRON 1 DEB *
ELEKTRON 1 DEB *, 18589 is space debris in LEO originally from a launch on Thu, 30 Jan 1964 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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 ELEKTRON 1 DEB * Date of exalting 30.01.1964y. Average height of ISS ELEKTRON 1 DEB * hundred 2942.24 km. Average velocity ELEKTRON 1 DEB * is 23543.61 km/h. Inclination ELEKTRON 1 DEB * satellite 58.95°.TLE
Average velocity ELEKTRON 1 DEB *
Average inclination ELEKTRON 1 DEB *
Mean right ascension of the ascending node (RAAN) ELEKTRON 1 DEB *
Mean argument of perigee ELEKTRON 1 DEB *
Mean semi-major axis of the orbit ELEKTRON 1 DEB *
Mean orbital eccentricity ELEKTRON 1 DEB *
ISS
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