DNEPR 1 R/B
Satellite information DNEPR 1 R/B
| Spacetrack Directory Name | DNEPR 1 R/B |
| Follow DNEPR 1 R/B | DNEPR 1 R/B Tracker |
| Pass predictions DNEPR 1 R/B | Pass predictions DNEPR 1 R/B |
| Orbit launches |
2000-09-26 (25 years ago)
|
| Days in orbit | 9474 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| WWW | Here |
| Perigee | 578 km |
| Apogee | 1344 km |
| Orbit slope (inclination) | 64.56° |
| Laps per day | 14 |
| Height DNEPR 1 R/B | 975.97 km |
Additional information DNEPR 1 R/B
DNEPR 1 R/B, 26550 is space debris in LEO originally from a launch on Tue, 26 Sep 2000 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 DNEPR 1 R/B Date of exalting 26.09.2000y. Average height of ISS DNEPR 1 R/B hundred 975.97 km. Average velocity DNEPR 1 R/B is 26515.44 km/h. Inclination DNEPR 1 R/B satellite 64.56°.TLE
Average velocity DNEPR 1 R/B
Average inclination DNEPR 1 R/B
Mean right ascension of the ascending node (RAAN) DNEPR 1 R/B
Mean argument of perigee DNEPR 1 R/B
Mean semi-major axis of the orbit DNEPR 1 R/B
Mean orbital eccentricity DNEPR 1 R/B
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