IRIDIUM 105
Satellite information IRIDIUM 105 - Iridium Next SV105
| Spacetrack Directory Name | IRIDIUM 105 |
| Alternative name | Iridium Next SV105 |
| Group | IRIDIUM |
| Follow IRIDIUM 105 | IRIDIUM 105 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 105 | Pass predictions IRIDIUM 105 |
| Orbit launches |
2017-01-14 (9 years ago)
|
| Days in orbit | 3556 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| Categories | |
| Perigee | 776 km |
| Apogee | 779 km |
| Orbit slope (inclination) | 86.4° |
| Laps per day | 14 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 105 | 789.7 km |
Additional information IRIDIUM 105
IRIDIUM 105 (also known as Iridium Next SV105) is a communication and traffic monitoring satellite manufactured by OATKGA for IRIDS (Iridium LLC). It was launched on January 14, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle. The satellite measures 3.1 meters in length with a diameter of 1.5 meters and spans 9.4 meters. Equipped with L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and an AIS-receiver, the satellite has a dry mass of 700 kg and a launch mass of 860 kg. Its power source includes two deployable solar arrays and batteries. The satellite is designed for a lifespan of 10 years with plans to extend it up to 15 years.
satellite IRIDIUM 105 Date of exalting 14.01.2017y. Average height of ISS IRIDIUM 105 hundred 789.7 km. Average velocity IRIDIUM 105 is 26857.28 km/h. Inclination IRIDIUM 105 satellite 86.4°.TLE
Average velocity IRIDIUM 105
Average inclination IRIDIUM 105
Mean right ascension of the ascending node (RAAN) IRIDIUM 105
Mean argument of perigee IRIDIUM 105
Mean semi-major axis of the orbit IRIDIUM 105
Mean orbital eccentricity IRIDIUM 105
ISS
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