ESSA 4 (TOS-B)
Satellite information ESSA 4 (TOS-B)
| Spacetrack Directory Name | ESSA 4 (TOS-B) |
| Follow ESSA 4 (TOS-B) | ESSA 4 (TOS-B) Tracker |
| Pass predictions ESSA 4 (TOS-B) | Pass predictions ESSA 4 (TOS-B) |
| Orbit launches |
1967-01-26 (59 years ago)
|
| Days in orbit | 21770 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 1326 km |
| Apogee | 1439 km |
| Orbit slope (inclination) | 102.08° |
| Laps per day | 13 |
| Height ESSA 4 (TOS-B) | 1394.02 km |
Additional information ESSA 4 (TOS-B)
ESSA 4 (TOS-B), 2657 is a payload satellite owned by ESSA (US) in SSO that was launched on Thu, 26 Jan 1967 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 4 (TOS-B) Date of exalting 26.01.1967y. Average height of ISS ESSA 4 (TOS-B) hundred 1394.02 km. Average velocity ESSA 4 (TOS-B) is 25792.09 km/h. Inclination ESSA 4 (TOS-B) satellite 102.08°.TLE
Average velocity ESSA 4 (TOS-B)
Average inclination ESSA 4 (TOS-B)
Mean right ascension of the ascending node (RAAN) ESSA 4 (TOS-B)
Mean argument of perigee ESSA 4 (TOS-B)
Mean semi-major axis of the orbit ESSA 4 (TOS-B)
Mean orbital eccentricity ESSA 4 (TOS-B)
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