ITOS 1 (TIROS M)
Satellite information ITOS 1 (TIROS M)
| Spacetrack Directory Name | ITOS 1 (TIROS M) |
| Follow ITOS 1 (TIROS M) | ITOS 1 (TIROS M) Tracker |
| Pass predictions ITOS 1 (TIROS M) | Pass predictions ITOS 1 (TIROS M) |
| Orbit launches |
1970-01-23 (56 years ago)
|
| Days in orbit | 20676 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1434 km |
| Apogee | 1478 km |
| Orbit slope (inclination) | 101.37° |
| Laps per day | 13 |
| Height ITOS 1 (TIROS M) | 1467.28 km |
Additional information ITOS 1 (TIROS M)
ITOS 1 (TIROS M), 4320 is a payload satellite owned by ESSA (US) in SSO that was launched on Fri, 23 Jan 1970 UTC via a THOR DELTA N6 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 ITOS 1 (TIROS M) Date of exalting 23.01.1970y. Average height of ISS ITOS 1 (TIROS M) hundred 1467.28 km. Average velocity ITOS 1 (TIROS M) is 25671.2 km/h. Inclination ITOS 1 (TIROS M) satellite 101.37°.TLE
Average velocity ITOS 1 (TIROS M)
Average inclination ITOS 1 (TIROS M)
Mean right ascension of the ascending node (RAAN) ITOS 1 (TIROS M)
Mean argument of perigee ITOS 1 (TIROS M)
Mean semi-major axis of the orbit ITOS 1 (TIROS M)
Mean orbital eccentricity ITOS 1 (TIROS M)
ISS
Buy us a coffee!
