IRIDIUM 39
Satellite information IRIDIUM 39
| Spacetrack Directory Name | IRIDIUM 39 |
| Follow IRIDIUM 39 | IRIDIUM 39 Tracker |
| Pass predictions IRIDIUM 39 | Pass predictions IRIDIUM 39 |
| Orbit launches |
1997-11-09 (28 years ago)
|
| Days in orbit | 10516 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Categories | |
| Perigee | 724 km |
| Apogee | 751 km |
| Orbit slope (inclination) | 86.39° |
| Laps per day | 15 |
| Height IRIDIUM 39 | 738.5 km |
Additional information IRIDIUM 39
IRIDIUM 39, 25042 is a payload satellite owned by Iridium (US) in LEO that was launched on Sun, 09 Nov 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 39 Date of exalting 09.11.1997y. Average height of ISS IRIDIUM 39 hundred 738.5 km. Average velocity IRIDIUM 39 is 26953.72 km/h. Inclination IRIDIUM 39 satellite 86.39°.TLE
Average velocity IRIDIUM 39
Average inclination IRIDIUM 39
Mean right ascension of the ascending node (RAAN) IRIDIUM 39
Mean argument of perigee IRIDIUM 39
Mean semi-major axis of the orbit IRIDIUM 39
Mean orbital eccentricity IRIDIUM 39
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