IRIDIUM 26
Satellite information IRIDIUM 26
| Spacetrack Directory Name | IRIDIUM 26 |
| Follow IRIDIUM 26 | IRIDIUM 26 Tracker |
| Pass predictions IRIDIUM 26 | Pass predictions IRIDIUM 26 |
| Orbit launches |
1997-08-21 (29 years ago)
|
| Days in orbit | 10596 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Categories | |
| Perigee | 772 km |
| Apogee | 775 km |
| Orbit slope (inclination) | 86.39° |
| Laps per day | 14 |
| Height IRIDIUM 26 | 778.92 km |
Additional information IRIDIUM 26
IRIDIUM 26, 24903 is a payload satellite owned by Iridium (US) in LEO that was launched on Thu, 21 Aug 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 26 Date of exalting 21.08.1997y. Average height of ISS IRIDIUM 26 hundred 778.92 km. Average velocity IRIDIUM 26 is 26877.48 km/h. Inclination IRIDIUM 26 satellite 86.39°.TLE
Average velocity IRIDIUM 26
Average inclination IRIDIUM 26
Mean right ascension of the ascending node (RAAN) IRIDIUM 26
Mean argument of perigee IRIDIUM 26
Mean semi-major axis of the orbit IRIDIUM 26
Mean orbital eccentricity IRIDIUM 26
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