TIROS 4
Satellite information TIROS 4 - TIROS-D
| Spacetrack Directory Name | TIROS 4 |
| Alternative name | TIROS-D |
| Follow TIROS 4 | TIROS 4 Tracker |
| Pass predictions TIROS 4 | Pass predictions TIROS 4 |
| Orbit launches |
1962-02-08 (64 years ago)
|
| Days in orbit | 23591 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Satellite |
| Perigee | 684 km |
| Apogee | 796 km |
| Orbit slope (inclination) | 48.3° |
| Laps per day | 14 |
| Height TIROS 4 | 740.42 km |
Additional information TIROS 4
TIROS 4, 226 is a payload satellite owned by GSFC (US) in LEO that was launched on Thu, 08 Feb 1962 UTC via a THOR DELTA launch vehicle from the Air Force Eastern Test Range (AFETR). 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 4 Date of exalting 08.02.1962y. Average height of ISS TIROS 4 hundred 740.42 km. Average velocity TIROS 4 is 26952.88 km/h. Inclination TIROS 4 satellite 48.3°.TLE
Average velocity TIROS 4
Average inclination TIROS 4
Mean right ascension of the ascending node (RAAN) TIROS 4
Mean argument of perigee TIROS 4
Mean semi-major axis of the orbit TIROS 4
Mean orbital eccentricity TIROS 4
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