ELEKTRON 3 DEB
Satellite information ELEKTRON 3 DEB
| Spacetrack Directory Name | ELEKTRON 3 DEB |
| Follow ELEKTRON 3 DEB | ELEKTRON 3 DEB Tracker |
| Pass predictions ELEKTRON 3 DEB | Pass predictions ELEKTRON 3 DEB |
| Orbit launches |
1964-07-10 (62 years ago)
|
| Days in orbit | 22757 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 408 km |
| Apogee | 5965 km |
| Orbit slope (inclination) | 60.83° |
| Laps per day | 9 |
| Height ELEKTRON 3 DEB | 3517.97 km |
Additional information ELEKTRON 3 DEB
ELEKTRON 3 DEB, 29008 is space debris originally from a launch on Fri, 10 Jul 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 3 DEB Date of exalting 10.07.1964y. Average height of ISS ELEKTRON 3 DEB hundred 3517.97 km. Average velocity ELEKTRON 3 DEB is 22836.64 km/h. Inclination ELEKTRON 3 DEB satellite 60.83°.TLE
Average velocity ELEKTRON 3 DEB
Average inclination ELEKTRON 3 DEB
Mean right ascension of the ascending node (RAAN) ELEKTRON 3 DEB
Mean argument of perigee ELEKTRON 3 DEB
Mean semi-major axis of the orbit ELEKTRON 3 DEB
Mean orbital eccentricity ELEKTRON 3 DEB
ISS
Buy us a coffee!
