SECOR 9 (EGRS 9)
Satellite information SECOR 9 (EGRS 9)
| Spacetrack Directory Name | SECOR 9 (EGRS 9) |
| Follow SECOR 9 (EGRS 9) | SECOR 9 (EGRS 9) Tracker |
| Pass predictions SECOR 9 (EGRS 9) | Pass predictions SECOR 9 (EGRS 9) |
| Orbit launches |
1967-06-29 (59 years ago)
|
| Days in orbit | 21616 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 3795 km |
| Apogee | 3947 km |
| Orbit slope (inclination) | 89.98° |
| Laps per day | 8 |
| Height SECOR 9 (EGRS 9) | 3883.41 km |
Additional information SECOR 9 (EGRS 9)
SECOR 9 (EGRS 9), 2861 is an American payload satellite in LEO that was launched on Thu, 29 Jun 1967 UTC via a THOR BURNER 2 launch vehicle from the Air Force Western Test Range (AFWTR). 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 SECOR 9 (EGRS 9) Date of exalting 29.06.1967y. Average height of ISS SECOR 9 (EGRS 9) hundred 3883.41 km. Average velocity SECOR 9 (EGRS 9) is 22445.22 km/h. Inclination SECOR 9 (EGRS 9) satellite 89.98°.TLE
Average velocity SECOR 9 (EGRS 9)
Average inclination SECOR 9 (EGRS 9)
Mean right ascension of the ascending node (RAAN) SECOR 9 (EGRS 9)
Mean argument of perigee SECOR 9 (EGRS 9)
Mean semi-major axis of the orbit SECOR 9 (EGRS 9)
Mean orbital eccentricity SECOR 9 (EGRS 9)
ISS
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