IRIDIUM 24
Satellite information IRIDIUM 24
| Spacetrack Directory Name | IRIDIUM 24 |
| Follow IRIDIUM 24 | IRIDIUM 24 Tracker |
| Pass predictions IRIDIUM 24 | Pass predictions IRIDIUM 24 |
| Orbit launches |
1997-12-20 (28 years ago)
|
| Days in orbit | 10475 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Categories | |
| Perigee | 749 km |
| Apogee | 768 km |
| Orbit slope (inclination) | 86.39° |
| Laps per day | 14 |
| Height IRIDIUM 24 | 762.32 km |
Additional information IRIDIUM 24
IRIDIUM 24, 25105 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 20 Dec 1997 UTC via a DELTA 7920-10C 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 IRIDIUM 24 Date of exalting 20.12.1997y. Average height of ISS IRIDIUM 24 hundred 762.32 km. Average velocity IRIDIUM 24 is 26908.67 km/h. Inclination IRIDIUM 24 satellite 86.39°.TLE
Average velocity IRIDIUM 24
Average inclination IRIDIUM 24
Mean right ascension of the ascending node (RAAN) IRIDIUM 24
Mean argument of perigee IRIDIUM 24
Mean semi-major axis of the orbit IRIDIUM 24
Mean orbital eccentricity IRIDIUM 24
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