IRIDIUM 100
Satellite information IRIDIUM 100 - Iridium Next SV127
| Spacetrack Directory Name | IRIDIUM 100 |
| Alternative name | Iridium Next SV127 |
| Group | IRIDIUM |
| Follow IRIDIUM 100 | IRIDIUM 100 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 100 | Pass predictions IRIDIUM 100 |
| 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 100 | 789.86 km |
Additional information IRIDIUM 100
The IRIDIUM 100 (also known as Iridium Next SV127) satellite was launched on October 9, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle by owner IRIDS. It has a configuration of ELiTeBus-1000 and measures 3.1 meters in length with a diameter of 1.5 meters and a span of 9.4 meters. The satellites dry mass is 700 kg, and its launch mass was 860 kg. It is equipped with an L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and AIS-receiver (on 58 satellites). Its power comes from two deployable solar arrays and batteries. The mission of IRIDIUM 100 is for communication and traffic monitoring purposes, designed to operate for 10 years with a planned lifetime extension to 15 years.
satellite IRIDIUM 100 Date of exalting 09.10.2017y. Average height of ISS IRIDIUM 100 hundred 789.86 km. Average velocity IRIDIUM 100 is 26856.99 km/h. Inclination IRIDIUM 100 satellite 86.4°.TLE
Average velocity IRIDIUM 100
Average inclination IRIDIUM 100
Mean right ascension of the ascending node (RAAN) IRIDIUM 100
Mean argument of perigee IRIDIUM 100
Mean semi-major axis of the orbit IRIDIUM 100
Mean orbital eccentricity IRIDIUM 100
ISS
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