SOLRAD 1 (GREB)
Satellite information SOLRAD 1 (GREB) - GRAB 1
| Spacetrack Directory Name | SOLRAD 1 (GREB) |
| Alternative name | GRAB 1 |
| Follow SOLRAD 1 (GREB) | SOLRAD 1 (GREB) Tracker |
| Pass predictions SOLRAD 1 (GREB) | Pass predictions SOLRAD 1 (GREB) |
| Orbit launches |
1960-06-22 g.05:54 (66 years ago)
|
| Days in orbit | 24165 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Satellite |
| Perigee | 577 km |
| Apogee | 878 km |
| Orbit slope (inclination) | 66.69° |
| Laps per day | 15 |
| Height SOLRAD 1 (GREB) | 720.21 km |
Additional information SOLRAD 1 (GREB)
SOLRAD 1 (GREB), 46 is a payload satellite owned by NRL (US) in LEO that was launched on Wed, 22 Jun 1960 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 1 (GREB) Date of exalting 22.06.1960y. Average height of ISS SOLRAD 1 (GREB) hundred 720.21 km. Average velocity SOLRAD 1 (GREB) is 26990.49 km/h. Inclination SOLRAD 1 (GREB) satellite 66.69°.TLE
Average velocity SOLRAD 1 (GREB)
Average inclination SOLRAD 1 (GREB)
Mean right ascension of the ascending node (RAAN) SOLRAD 1 (GREB)
Mean argument of perigee SOLRAD 1 (GREB)
Mean semi-major axis of the orbit SOLRAD 1 (GREB)
Mean orbital eccentricity SOLRAD 1 (GREB)
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