SECOR 8 (EGRS 8)
Satellite information SECOR 8 (EGRS 8)
| Spacetrack Directory Name | SECOR 8 (EGRS 8) |
| Follow SECOR 8 (EGRS 8) | SECOR 8 (EGRS 8) Tracker |
| Pass predictions SECOR 8 (EGRS 8) | Pass predictions SECOR 8 (EGRS 8) |
| Orbit launches |
1966-10-05 (59 years ago)
|
| Days in orbit | 21883 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 3678 km |
| Apogee | 3710 km |
| Orbit slope (inclination) | 89.85° |
| Laps per day | 9 |
| Height SECOR 8 (EGRS 8) | 3705.51 km |
Additional information SECOR 8 (EGRS 8)
SECOR 8 (EGRS 8), 2520 is an American payload satellite in LEO that was launched on Wed, 05 Oct 1966 UTC via an ATLAS SLV-3 AGENA D 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 8 (EGRS 8) Date of exalting 05.10.1966y. Average height of ISS SECOR 8 (EGRS 8) hundred 3705.51 km. Average velocity SECOR 8 (EGRS 8) is 22642.41 km/h. Inclination SECOR 8 (EGRS 8) satellite 89.85°.TLE
Average velocity SECOR 8 (EGRS 8)
Average inclination SECOR 8 (EGRS 8)
Mean right ascension of the ascending node (RAAN) SECOR 8 (EGRS 8)
Mean argument of perigee SECOR 8 (EGRS 8)
Mean semi-major axis of the orbit SECOR 8 (EGRS 8)
Mean orbital eccentricity SECOR 8 (EGRS 8)
ISS
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