IRIDIUM 155
Satellite information IRIDIUM 155 - Iridium Next SV155
| Spacetrack Directory Name | IRIDIUM 155 |
| Alternative name | Iridium Next SV155 |
| Group | IRIDIUM |
| Follow IRIDIUM 155 | IRIDIUM 155 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 155 | Pass predictions IRIDIUM 155 |
| Orbit launches |
2018-07-25 (8 years ago)
|
| Days in orbit | 2999 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| WWW | Here |
| Categories | |
| Perigee | 776 km |
| Apogee | 779 km |
| Orbit slope (inclination) | 86.4° |
| Laps per day | 14 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 155 | 789.86 km |
Additional information IRIDIUM 155
IRIDIUM 155 (also known as Iridium Next SV155) is a communication and traffic monitoring satellite launched on July 25, 2018, from AFWTR SLC4E using a Falcon 9 launch vehicle. The spacecraft has dimensions of 3.1 meters in length and 1.5 meters in diameter with a span of 9.4 meters. It features an ELiTeBus-1000 configuration and carries a L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and AIS-receiver (part of a set on 58 satellites). The satellite has a dry mass of 700 kg and a launch mass of 860 kg. It is powered by two deployable solar arrays and batteries. Designed for a lifetime of 10 years with plans for an extended operation up to 15 years, IRIDIUM 155 is owned by IRIDS and manufactured by NGISGA. The satellites shape is described as a half hex prism with two pans.
satellite IRIDIUM 155 Date of exalting 25.07.2018y. Average height of ISS IRIDIUM 155 hundred 789.86 km. Average velocity IRIDIUM 155 is 26856.99 km/h. Inclination IRIDIUM 155 satellite 86.4°.TLE
Average velocity IRIDIUM 155
Average inclination IRIDIUM 155
Mean right ascension of the ascending node (RAAN) IRIDIUM 155
Mean argument of perigee IRIDIUM 155
Mean semi-major axis of the orbit IRIDIUM 155
Mean orbital eccentricity IRIDIUM 155
ISS
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