IRIDIUM 107
Satellite information IRIDIUM 107 - Iridium Next SV107
| Spacetrack Directory Name | IRIDIUM 107 |
| Alternative name | Iridium Next SV107 |
| Group | IRIDIUM |
| Follow IRIDIUM 107 | IRIDIUM 107 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 107 | Pass predictions IRIDIUM 107 |
| Orbit launches |
2017-10-09 (9 years ago)
|
| Days in orbit | 3288 |
| 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 107 | 789.86 km |
Additional information IRIDIUM 107
IRIDIUM 107 (also known as Iridium Next SV107) is a communication and traffic monitoring satellite launched on October 9, 2017, from Vandenberg Air Force Base SLC4E using a Falcon 9 launch vehicle. The spacecraft has dimensions of 3.1 meters in length, 1.5 meters in diameter, and a span of 9.4 meters. It is equipped with L-band payload, Ka-band cross-links and downlinks, an ADS-B payload, and AIS-receiver (part of a set on 58 satellites). The satellite has a dry mass of 700 kilograms and was manufactured by OATKGA for the owner IRIDS. Power is supplied through two deployable solar arrays and batteries. Its design life expectancy is 10 years with plans for an extended operation up to 15 years.
satellite IRIDIUM 107 Date of exalting 09.10.2017y. Average height of ISS IRIDIUM 107 hundred 789.86 km. Average velocity IRIDIUM 107 is 26856.99 km/h. Inclination IRIDIUM 107 satellite 86.4°.TLE
Average velocity IRIDIUM 107
Average inclination IRIDIUM 107
Mean right ascension of the ascending node (RAAN) IRIDIUM 107
Mean argument of perigee IRIDIUM 107
Mean semi-major axis of the orbit IRIDIUM 107
Mean orbital eccentricity IRIDIUM 107
ISS
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