ESSA 2 (OT-2)
Satellite information ESSA 2 (OT-2)
| Spacetrack Directory Name | ESSA 2 (OT-2) |
| Follow ESSA 2 (OT-2) | ESSA 2 (OT-2) Tracker |
| Pass predictions ESSA 2 (OT-2) | Pass predictions ESSA 2 (OT-2) |
| Orbit launches |
1966-02-28 (60 years ago)
|
| Days in orbit | 22109 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 1354 km |
| Apogee | 1415 km |
| Orbit slope (inclination) | 101.22° |
| Laps per day | 13 |
| Height ESSA 2 (OT-2) | 1395.9 km |
Additional information ESSA 2 (OT-2)
ESSA 2 (OT-2), 2091 is a payload satellite owned by ESSA (US) in SSO that was launched on Mon, 28 Feb 1966 UTC via a THOR DELTA E 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 2 (OT-2) Date of exalting 28.02.1966y. Average height of ISS ESSA 2 (OT-2) hundred 1395.9 km. Average velocity ESSA 2 (OT-2) is 25788.78 km/h. Inclination ESSA 2 (OT-2) satellite 101.22°.TLE
Average velocity ESSA 2 (OT-2)
Average inclination ESSA 2 (OT-2)
Mean right ascension of the ascending node (RAAN) ESSA 2 (OT-2)
Mean argument of perigee ESSA 2 (OT-2)
Mean semi-major axis of the orbit ESSA 2 (OT-2)
Mean orbital eccentricity ESSA 2 (OT-2)
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