SL-6 R/B(2)
Satellite information SL-6 R/B(2) - Blok-2BL 12-695
| Spacetrack Directory Name | SL-6 R/B(2) |
| Alternative name | Blok-2BL 12-695 |
| Follow SL-6 R/B(2) | SL-6 R/B(2) Tracker |
| Pass predictions SL-6 R/B(2) | Pass predictions SL-6 R/B(2) |
| Orbit launches |
1994-08-05 (32 years ago)
|
| Days in orbit | 11729 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Type | Rocket body |
| Perigee | 4000 km |
| Apogee | 35791 km |
| Orbit slope (inclination) | 67.72° |
| Laps per day | 2 |
| Height SL-6 R/B(2) | 23741.35 km |
Additional information SL-6 R/B(2)
SL-6 R/B(2), 23197 is space debris in HEO originally from a launch on Fri, 05 Aug 1994 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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 SL-6 R/B(2) Date of exalting 05.08.1994y. Average height of ISS SL-6 R/B(2) hundred 23741.35 km. Average velocity SL-6 R/B(2) is 12925.6 km/h. Inclination SL-6 R/B(2) satellite 67.72°.TLE
Average velocity SL-6 R/B(2)
Average inclination SL-6 R/B(2)
Mean right ascension of the ascending node (RAAN) SL-6 R/B(2)
Mean argument of perigee SL-6 R/B(2)
Mean semi-major axis of the orbit SL-6 R/B(2)
Mean orbital eccentricity SL-6 R/B(2)
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