ESSA 8 (TOS-F)
Satellite information ESSA 8 (TOS-F)
| Spacetrack Directory Name | ESSA 8 (TOS-F) |
| Follow ESSA 8 (TOS-F) | ESSA 8 (TOS-F) Tracker |
| Pass predictions ESSA 8 (TOS-F) | Pass predictions ESSA 8 (TOS-F) |
| Orbit launches |
1968-12-15 (57 years ago)
|
| Days in orbit | 21081 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1414 km |
| Apogee | 1463 km |
| Orbit slope (inclination) | 101.71° |
| Laps per day | 13 |
| Height ESSA 8 (TOS-F) | 1449.88 km |
Additional information ESSA 8 (TOS-F)
ESSA 8 (TOS-F), 3615 is a payload satellite owned by ESSA (US) in SSO that was launched on Sun, 15 Dec 1968 UTC via a THOR DELTA N 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 8 (TOS-F) Date of exalting 15.12.1968y. Average height of ISS ESSA 8 (TOS-F) hundred 1449.88 km. Average velocity ESSA 8 (TOS-F) is 25699.6 km/h. Inclination ESSA 8 (TOS-F) satellite 101.7°.TLE
Average velocity ESSA 8 (TOS-F)
Average inclination ESSA 8 (TOS-F)
Mean right ascension of the ascending node (RAAN) ESSA 8 (TOS-F)
Mean argument of perigee ESSA 8 (TOS-F)
Mean semi-major axis of the orbit ESSA 8 (TOS-F)
Mean orbital eccentricity ESSA 8 (TOS-F)
ISS
Buy us a coffee!
