RADIATION SAT (5E 1)
Satellite information RADIATION SAT (5E 1) - 5E-1
| Spacetrack Directory Name | RADIATION SAT (5E 1) |
| Alternative name | 5E-1 |
| Follow RADIATION SAT (5E 1) | RADIATION SAT (5E 1) Tracker |
| Pass predictions RADIATION SAT (5E 1) | Pass predictions RADIATION SAT (5E 1) |
| Orbit launches |
1963-09-28 (63 years ago)
|
| Days in orbit | 23038 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| Perigee | 1062 km |
| Apogee | 1120 km |
| Orbit slope (inclination) | 89.96° |
| Laps per day | 13 |
| Height RADIATION SAT (5E 1) | 1102.11 km |
Additional information RADIATION SAT (5E 1)
RADIATION SAT (5E 1), 671 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Sat, 28 Sep 1963 UTC via a THOR ABLESTAR 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 RADIATION SAT (5E 1) Date of exalting 28.09.1963y. Average height of ISS RADIATION SAT (5E 1) hundred 1102.11 km. Average velocity RADIATION SAT (5E 1) is 26290.31 km/h. Inclination RADIATION SAT (5E 1) satellite 89.97°.TLE
Average velocity RADIATION SAT (5E 1)
Average inclination RADIATION SAT (5E 1)
Mean right ascension of the ascending node (RAAN) RADIATION SAT (5E 1)
Mean argument of perigee RADIATION SAT (5E 1)
Mean semi-major axis of the orbit RADIATION SAT (5E 1)
Mean orbital eccentricity RADIATION SAT (5E 1)
ISS
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