ISIS 2
Satellite information ISIS 2
| Spacetrack Directory Name | ISIS 2 |
| Follow ISIS 2 | ISIS 2 Tracker |
| Pass predictions ISIS 2 | Pass predictions ISIS 2 |
| Orbit launches |
1971-04-01 (55 years ago)
|
| Days in orbit | 20242 |
| Country/organisation of origin | Kanada (CA) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1356 km |
| Apogee | 1426 km |
| Orbit slope (inclination) | 88.16° |
| Laps per day | 13 |
| Height ISIS 2 | 1402.68 km |
Additional information ISIS 2
ISIS 2, 5104 is a payload satellite owned by CRC (CA) in LEO that was launched on Thu, 01 Apr 1971 UTC via a THOR DELTA E1 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 ISIS 2 Date of exalting 01.04.1971y. Average height of ISS ISIS 2 hundred 1402.68 km. Average velocity ISIS 2 is 25777.39 km/h. Inclination ISIS 2 satellite 88.17°.TLE
Average velocity ISIS 2
Average inclination ISIS 2
Mean right ascension of the ascending node (RAAN) ISIS 2
Mean argument of perigee ISIS 2
Mean semi-major axis of the orbit ISIS 2
Mean orbital eccentricity ISIS 2
ISS
Buy us a coffee!
