SPEKTR R
Satellite information SPEKTR R
| Spacetrack Directory Name | SPEKTR R |
| Follow SPEKTR R | SPEKTR R Tracker |
| Pass predictions SPEKTR R | Pass predictions SPEKTR R |
| Orbit launches |
2011-07-18 (15 years ago)
|
| Days in orbit | 5590 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| WWW | Here |
| Perigee | 11273 km |
| Apogee | 361032 km |
| Orbit slope (inclination) | 19.78° |
| Laps per day | 0 |
| Orbit | Elliptical (Cislunar) |
| Height SPEKTR R | 246667.53 km |
Additional information SPEKTR R
SPEKTR R, 37755 is a Commonwealth of Independent States-origin payload satellite in HEO that was launched on Mon, 18 Jul 2011 UTC via a ZENIT-3SLBF 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 SPEKTR R Date of exalting 18.07.2011y. Average height of ISS SPEKTR R hundred 246667.53 km. Average velocity SPEKTR R is 3848.18 km/h. Inclination SPEKTR R satellite 16.26°.TLE
Average velocity SPEKTR R
Average inclination SPEKTR R
Mean right ascension of the ascending node (RAAN) SPEKTR R
Mean argument of perigee SPEKTR R
Mean semi-major axis of the orbit SPEKTR R
Mean orbital eccentricity SPEKTR R
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