IRIDIUM 141
Satellite information IRIDIUM 141 - Iridium Next SV141
| Spacetrack Directory Name | IRIDIUM 141 |
| Alternative name | Iridium Next SV141 |
| Group | IRIDIUM |
| Follow IRIDIUM 141 | IRIDIUM 141 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 141 | Pass predictions IRIDIUM 141 |
| Orbit launches |
2017-12-23 (8 years ago)
|
| Days in orbit | 3213 |
| 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) | 86.39° |
| Laps per day | 14 |
| Height IRIDIUM 141 | 789.86 km |
Additional information IRIDIUM 141
IRIDIUM 141 (also known as Iridium Next SV141) is a communication and traffic monitoring satellite owned by IRIDS. Launched on December 23, 2017, from AFWTR SLC4E using the Falcon 9 launch vehicle, it has a dry mass of 700 kg and a launch mass of 860 kg. The satellite measures 3.1 meters in length with a diameter of 1.5 meters and a span of 9.4 meters. It is equipped with an L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and AIS-receiver technology. Its power system includes two deployable solar arrays and batteries. The design lifetime is planned for up to 15 years. Manufactured by OATKGA, the satellites shape is described as a half hex prism with two pans.
satellite IRIDIUM 141 Date of exalting 23.12.2017y. Average height of ISS IRIDIUM 141 hundred 789.86 km. Average velocity IRIDIUM 141 is 26856.99 km/h. Inclination IRIDIUM 141 satellite 86.4°.TLE
Average velocity IRIDIUM 141
Average inclination IRIDIUM 141
Mean right ascension of the ascending node (RAAN) IRIDIUM 141
Mean argument of perigee IRIDIUM 141
Mean semi-major axis of the orbit IRIDIUM 141
Mean orbital eccentricity IRIDIUM 141
ISS
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