IRIDIUM 4
Satellite information IRIDIUM 4
| Spacetrack Directory Name | IRIDIUM 4 |
| Follow IRIDIUM 4 | IRIDIUM 4 Tracker |
| Pass predictions IRIDIUM 4 | Pass predictions IRIDIUM 4 |
| Orbit launches |
1997-05-05 (29 years ago)
|
| Days in orbit | 10704 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Categories | |
| Perigee | 773 km |
| Apogee | 776 km |
| Orbit slope (inclination) | 86.4° |
| Laps per day | 14 |
| Height IRIDIUM 4 | 780 km |
Additional information IRIDIUM 4
Iridium 7 was a U.S. Iridium communications satellite. It was launched into low Earth orbit from Vandenberg Air Force Base at 14:55 GMT on 5 May 1997, by a Delta II 7920-10C carrier rocket. It was operated in Plane 4 of the Iridium satellite constellation, with an ascending node of 262.4°.It had a partial technical failure in 2009 and was subsequently paired with Iridium 51, and relegated to following it and managing traffic routing.
satellite IRIDIUM 4 Date of exalting 05.05.1997y. Average height of ISS IRIDIUM 4 hundred 780 km. Average velocity IRIDIUM 4 is 26875.45 km/h. Inclination IRIDIUM 4 satellite 86.4°.TLE
Average velocity IRIDIUM 4
Average inclination IRIDIUM 4
Mean right ascension of the ascending node (RAAN) IRIDIUM 4
Mean argument of perigee IRIDIUM 4
Mean semi-major axis of the orbit IRIDIUM 4
Mean orbital eccentricity IRIDIUM 4
ISS
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