OSIRIS-E
Satellite information OSIRIS-E
| Spacetrack Directory Name | OSIRIS-E |
| Follow OSIRIS-E | OSIRIS-E Tracker |
| Pass predictions OSIRIS-E | Pass predictions OSIRIS-E |
| Orbit launches |
2026-10-01 (one month ago)
|
| Days in orbit | 42 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 516 km |
| Apogee | 516 km |
| Orbit slope (inclination) | 97.44° |
| Laps per day | 15 |
| Height OSIRIS-E | 527.74 km |
Additional information OSIRIS-E
OSIRIS-E, 101108 is an American payload satellite in SSO that was launched on Thu, 01 Oct 2026 UTC launched from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft 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 OSIRIS-E Date of exalting 01.10.2026y. Average height of ISS OSIRIS-E hundred 527.74 km. Average velocity OSIRIS-E is 27362.11 km/h. Inclination OSIRIS-E satellite 97.44°.TLE
Average velocity OSIRIS-E
Average inclination OSIRIS-E
Mean right ascension of the ascending node (RAAN) OSIRIS-E
Mean argument of perigee OSIRIS-E
Mean semi-major axis of the orbit OSIRIS-E
Mean orbital eccentricity OSIRIS-E
ISS
Buy us a coffee!
