ELEKTRON 1 DEB
Satellite information ELEKTRON 1 DEB - Elektron-1 motor
| Spacetrack Directory Name | ELEKTRON 1 DEB |
| Alternative name | Elektron-1 motor |
| 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) |
| Type | Debris |
| Perigee | 393 km |
| Apogee | 3152 km |
| Orbit slope (inclination) | 60.75° |
| Laps per day | 13 |
| Height ELEKTRON 1 DEB | 1530.15 km |
Additional information ELEKTRON 1 DEB
ELEKTRON 1 DEB, 750 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 1530.15 km. Average velocity ELEKTRON 1 DEB is 25567.94 km/h. Inclination ELEKTRON 1 DEB satellite 60.74°.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
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