SOLRAD 3/INJUN 1
Satellite information SOLRAD 3/INJUN 1 - SOLRAD 3 & INJUN 1
| Spacetrack Directory Name | SOLRAD 3/INJUN 1 |
| Alternative name | SOLRAD 3 & INJUN 1 |
| Follow SOLRAD 3/INJUN 1 | SOLRAD 3/INJUN 1 Tracker |
| Pass predictions SOLRAD 3/INJUN 1 | Pass predictions SOLRAD 3/INJUN 1 |
| Orbit launches |
1961-06-29 g.04:22 (65 years ago)
|
| Days in orbit | 23859 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Satellite |
| Perigee | 868 km |
| Apogee | 991 km |
| Orbit slope (inclination) | 66.81° |
| Laps per day | 14 |
| Height SOLRAD 3/INJUN 1 | 938.01 km |
Additional information SOLRAD 3/INJUN 1
SOLRAD 3/INJUN 1, 117 is an American payload satellite in LEO that was launched on Thu, 29 Jun 1961 UTC via a THOR ABLESTAR 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 SOLRAD 3/INJUN 1 Date of exalting 29.06.1961y. Average height of ISS SOLRAD 3/INJUN 1 hundred 938.01 km. Average velocity SOLRAD 3/INJUN 1 is 26584.38 km/h. Inclination SOLRAD 3/INJUN 1 satellite 66.81°.TLE
Average velocity SOLRAD 3/INJUN 1
Average inclination SOLRAD 3/INJUN 1
Mean right ascension of the ascending node (RAAN) SOLRAD 3/INJUN 1
Mean argument of perigee SOLRAD 3/INJUN 1
Mean semi-major axis of the orbit SOLRAD 3/INJUN 1
Mean orbital eccentricity SOLRAD 3/INJUN 1
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