EKRAN 2 DEB
Satellite information EKRAN 2 DEB
| Spacetrack Directory Name | EKRAN 2 DEB |
| Follow EKRAN 2 DEB | EKRAN 2 DEB Tracker |
| Pass predictions EKRAN 2 DEB | Pass predictions EKRAN 2 DEB |
| Orbit launches |
1977-09-20 (49 years ago)
|
| Days in orbit | 17917 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 35731 km |
| Apogee | 35784 km |
| Orbit slope (inclination) | 3.85° |
| Laps per day | 1 |
| Height EKRAN 2 DEB | 35757.43 km |
Additional information EKRAN 2 DEB
EKRAN 2 DEB, 11581 is space debris in GEO originally from a launch on Tue, 20 Sep 1977 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 EKRAN 2 DEB Date of exalting 20.09.1977y. Average height of ISS EKRAN 2 DEB hundred 35757.43 km. Average velocity EKRAN 2 DEB is 11072.72 km/h. Inclination EKRAN 2 DEB satellite 3.93°.TLE
Average velocity EKRAN 2 DEB
Average inclination EKRAN 2 DEB
Mean right ascension of the ascending node (RAAN) EKRAN 2 DEB
Mean argument of perigee EKRAN 2 DEB
Mean semi-major axis of the orbit EKRAN 2 DEB
Mean orbital eccentricity EKRAN 2 DEB
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