COSMOS 626
Satellite information COSMOS 626
| Spacetrack Directory Name | COSMOS 626 |
| Follow COSMOS 626 | COSMOS 626 Tracker |
| Pass predictions COSMOS 626 | Pass predictions COSMOS 626 |
| Orbit launches |
1973-12-27 (52 years ago)
|
| Days in orbit | 19286 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 905 km |
| Apogee | 985 km |
| Orbit slope (inclination) | 65.44° |
| Laps per day | 14 |
| Height COSMOS 626 | 954.04 km |
Additional information COSMOS 626
COSMOS 626, 7005 is a payload satellite owned by VMF (CIS) in LEO that was launched on Thu, 27 Dec 1973 UTC via a TSIKLON-2 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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 COSMOS 626 Date of exalting 27.12.1973y. Average height of ISS COSMOS 626 hundred 954.04 km. Average velocity COSMOS 626 is 26555.47 km/h. Inclination COSMOS 626 satellite 65.44°.TLE
Average velocity COSMOS 626
Average inclination COSMOS 626
Mean right ascension of the ascending node (RAAN) COSMOS 626
Mean argument of perigee COSMOS 626
Mean semi-major axis of the orbit COSMOS 626
Mean orbital eccentricity COSMOS 626
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