TIROS 8
Satellite information TIROS 8
| Spacetrack Directory Name | TIROS 8 |
| Follow TIROS 8 | TIROS 8 Tracker |
| Pass predictions TIROS 8 | Pass predictions TIROS 8 |
| Orbit launches |
1963-12-21 (62 years ago)
|
| Days in orbit | 22910 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 647 km |
| Apogee | 678 km |
| Orbit slope (inclination) | 58.49° |
| Laps per day | 15 |
| Height TIROS 8 | 658.84 km |
Additional information TIROS 8
TIROS 8, 716 is a payload satellite owned by GSFC (US) in LEO that was launched on Sat, 21 Dec 1963 UTC via a THOR DELTA B 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 TIROS 8 Date of exalting 21.12.1963y. Average height of ISS TIROS 8 hundred 658.84 km. Average velocity TIROS 8 is 27107.71 km/h. Inclination TIROS 8 satellite 58.49°.TLE
Average velocity TIROS 8
Average inclination TIROS 8
Mean right ascension of the ascending node (RAAN) TIROS 8
Mean argument of perigee TIROS 8
Mean semi-major axis of the orbit TIROS 8
Mean orbital eccentricity TIROS 8
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