IRIDIUM 162
Satellite information IRIDIUM 162 - Iridium Next SV162
| Spacetrack Directory Name | IRIDIUM 162 |
| Alternative name | Iridium Next SV162 |
| Group | IRIDIUM |
| Follow IRIDIUM 162 | IRIDIUM 162 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 162 | Pass predictions IRIDIUM 162 |
| Orbit launches |
2018-05-22 (8 years ago)
|
| Days in orbit | 3063 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| WWW | Here |
| Categories | |
| Perigee | 746 km |
| Apogee | 749 km |
| Orbit slope (inclination) | 86.45° |
| Laps per day | 14 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 162 | 759.88 km |
Additional information IRIDIUM 162
IRIDIUM 162 (also known as Iridium Next SV162) is a communication and traffic monitoring satellite owned by IRIDS and manufactured by OATKGA. Launched on May 22, 2018, from AFWTR SLC4E using the Falcon 9 launch vehicle, it has a configuration of ELiTeBus-1000 with dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters. The satellites dry mass is 700 kg, with a launch mass of 860 kg. It is equipped with L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and AIS-receiver (part of the equipment on 58 satellites). Its power comes from two deployable solar arrays and batteries. The satellites mission lifetime is designed for 10 years but planned to extend up to 15 years.
satellite IRIDIUM 162 Date of exalting 22.05.2018y. Average height of ISS IRIDIUM 162 hundred 759.88 km. Average velocity IRIDIUM 162 is 26913.34 km/h. Inclination IRIDIUM 162 satellite 86.45°.TLE
Average velocity IRIDIUM 162
Average inclination IRIDIUM 162
Mean right ascension of the ascending node (RAAN) IRIDIUM 162
Mean argument of perigee IRIDIUM 162
Mean semi-major axis of the orbit IRIDIUM 162
Mean orbital eccentricity IRIDIUM 162
ISS
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