IRIDIUM 57
Satellite information IRIDIUM 57
| Spacetrack Directory Name | IRIDIUM 57 |
| Follow IRIDIUM 57 | IRIDIUM 57 Tracker |
| Pass predictions IRIDIUM 57 | Pass predictions IRIDIUM 57 |
| Orbit launches |
1998-03-30 (28 years ago)
|
| Days in orbit | 10375 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Categories | |
| Perigee | 776 km |
| Apogee | 779 km |
| Orbit slope (inclination) | 86.4° |
| Laps per day | 14 |
| Height IRIDIUM 57 | 783.23 km |
Additional information IRIDIUM 57
IRIDIUM 57, 25273 is a payload satellite owned by Iridium (US) in LEO that was launched on Mon, 30 Mar 1998 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 57 Date of exalting 30.03.1998y. Average height of ISS IRIDIUM 57 hundred 783.23 km. Average velocity IRIDIUM 57 is 26869.47 km/h. Inclination IRIDIUM 57 satellite 86.4°.TLE
Average velocity IRIDIUM 57
Average inclination IRIDIUM 57
Mean right ascension of the ascending node (RAAN) IRIDIUM 57
Mean argument of perigee IRIDIUM 57
Mean semi-major axis of the orbit IRIDIUM 57
Mean orbital eccentricity IRIDIUM 57
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