RUBIN 4/SL-8
Satellite information RUBIN 4/SL-8 - RUBIN-4 & SL-8 R/B
| Spacetrack Directory Name | RUBIN 4/SL-8 |
| Alternative name | RUBIN-4 & SL-8 R/B |
| Follow RUBIN 4/SL-8 | RUBIN 4/SL-8 Tracker |
| Pass predictions RUBIN 4/SL-8 | Pass predictions RUBIN 4/SL-8 |
| Orbit launches |
2003-09-27 (22 years ago)
|
| Days in orbit | 8377 |
| Country/organisation of origin | Niemcy (GER) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Perigee | 666 km |
| Apogee | 687 km |
| Orbit slope (inclination) | 98.39° |
| Laps per day | 15 |
| Height RUBIN 4/SL-8 | 674.45 km |
Additional information RUBIN 4/SL-8
RUBIN 4/SL-8, 27940 is a payload satellite owned by KVR (DE) in SSO that was launched on Sat, 27 Sep 2003 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite RUBIN 4/SL-8 Date of exalting 27.09.2003y. Average height of ISS RUBIN 4/SL-8 hundred 674.45 km. Average velocity RUBIN 4/SL-8 is 27076.03 km/h. Inclination RUBIN 4/SL-8 satellite 98.39°.TLE
Average velocity RUBIN 4/SL-8
Average inclination RUBIN 4/SL-8
Mean right ascension of the ascending node (RAAN) RUBIN 4/SL-8
Mean argument of perigee RUBIN 4/SL-8
Mean semi-major axis of the orbit RUBIN 4/SL-8
Mean orbital eccentricity RUBIN 4/SL-8
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