ESSA 3 (TOS-A)
Satellite information ESSA 3 (TOS-A)
| Spacetrack Directory Name | ESSA 3 (TOS-A) |
| Follow ESSA 3 (TOS-A) | ESSA 3 (TOS-A) Tracker |
| Pass predictions ESSA 3 (TOS-A) | Pass predictions ESSA 3 (TOS-A) |
| Orbit launches |
1966-10-02 (59 years ago)
|
| Days in orbit | 21886 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1386 km |
| Apogee | 1486 km |
| Orbit slope (inclination) | 101.06° |
| Laps per day | 13 |
| Height ESSA 3 (TOS-A) | 1447.44 km |
Additional information ESSA 3 (TOS-A)
ESSA 3 (TOS-A), 2435 is a payload satellite owned by ESSA (US) in SSO that was launched on Sun, 02 Oct 1966 UTC via a THOR DELTA E 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 ESSA 3 (TOS-A) Date of exalting 02.10.1966y. Average height of ISS ESSA 3 (TOS-A) hundred 1447.44 km. Average velocity ESSA 3 (TOS-A) is 25703.78 km/h. Inclination ESSA 3 (TOS-A) satellite 101.07°.TLE
Average velocity ESSA 3 (TOS-A)
Average inclination ESSA 3 (TOS-A)
Mean right ascension of the ascending node (RAAN) ESSA 3 (TOS-A)
Mean argument of perigee ESSA 3 (TOS-A)
Mean semi-major axis of the orbit ESSA 3 (TOS-A)
Mean orbital eccentricity ESSA 3 (TOS-A)
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