IRIDIUM 28
Satellite information IRIDIUM 28
| Spacetrack Directory Name | IRIDIUM 28 |
| Follow IRIDIUM 28 | IRIDIUM 28 Tracker |
| Pass predictions IRIDIUM 28 | Pass predictions IRIDIUM 28 |
| Orbit launches |
1997-09-14 (28 years ago)
|
| Days in orbit | 10591 |
| Country/organisation of origin | USA (US) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Categories | |
| Perigee | 771 km |
| Apogee | 774 km |
| Orbit slope (inclination) | 86.4° |
| Laps per day | 14 |
| Height IRIDIUM 28 | 778.2 km |
Additional information IRIDIUM 28
IRIDIUM 28, 24948 is a payload satellite owned by Iridium (US) in LEO that was launched on Sun, 14 Sep 1997 UTC via a PROTON-K/17S40 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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 28 Date of exalting 14.09.1997y. Average height of ISS IRIDIUM 28 hundred 778.2 km. Average velocity IRIDIUM 28 is 26878.86 km/h. Inclination IRIDIUM 28 satellite 86.4°.TLE
Average velocity IRIDIUM 28
Average inclination IRIDIUM 28
Mean right ascension of the ascending node (RAAN) IRIDIUM 28
Mean argument of perigee IRIDIUM 28
Mean semi-major axis of the orbit IRIDIUM 28
Mean orbital eccentricity IRIDIUM 28
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