ESSA 1 (OT-3)
Satellite information ESSA 1 (OT-3)
| Spacetrack Directory Name | ESSA 1 (OT-3) |
| Follow ESSA 1 (OT-3) | ESSA 1 (OT-3) Tracker |
| Pass predictions ESSA 1 (OT-3) | Pass predictions ESSA 1 (OT-3) |
| Orbit launches |
1966-02-03 (60 years ago)
|
| Days in orbit | 22134 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 677 km |
| Apogee | 794 km |
| Orbit slope (inclination) | 97.81° |
| Laps per day | 14 |
| Height ESSA 1 (OT-3) | 743.15 km |
Additional information ESSA 1 (OT-3)
ESSA 1 (OT-3), 1982 is a payload satellite owned by ESSA (US) in SSO that was launched on Thu, 03 Feb 1966 UTC via a THOR DELTA C launch vehicle from the Air Force Eastern Test Range (AFETR). 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 ESSA 1 (OT-3) Date of exalting 03.02.1966y. Average height of ISS ESSA 1 (OT-3) hundred 743.15 km. Average velocity ESSA 1 (OT-3) is 26945.01 km/h. Inclination ESSA 1 (OT-3) satellite 97.81°.TLE
Average velocity ESSA 1 (OT-3)
Average inclination ESSA 1 (OT-3)
Mean right ascension of the ascending node (RAAN) ESSA 1 (OT-3)
Mean argument of perigee ESSA 1 (OT-3)
Mean semi-major axis of the orbit ESSA 1 (OT-3)
Mean orbital eccentricity ESSA 1 (OT-3)
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