IRIDIUM 153
Satellite information IRIDIUM 153 - Iridium Next SV153
| Spacetrack Directory Name | IRIDIUM 153 |
| Alternative name | Iridium Next SV153 |
| Group | IRIDIUM |
| Follow IRIDIUM 153 | IRIDIUM 153 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 153 | Pass predictions IRIDIUM 153 |
| 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 | 775 km |
| Apogee | 780 km |
| Orbit slope (inclination) | 86.39° |
| Laps per day | 14 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 153 | 789.87 km |
Additional information IRIDIUM 153
IRIDIUM 153, also known as Iridium Next SV153, is a communication and traffic monitoring satellite owned by IRIDS (Iridium LLC) and manufactured by OATKGA. Launched on December 23, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle, it has a design lifetime of 10 years with plans for a 15-year operational period. The satellite measures 3.1 meters in length and 1.5 meters in diameter, with a span of 9.4 meters, weighing 860 kg at launch and 700 kg dry mass. It is equipped with a L-band payload, Ka-band cross-links, downlinks, an ADS-B payload, and an AIS-receiver (part of a fleet of 58 satellites). Its power source includes two deployable solar arrays and batteries. The satellites shape is described as a half hexagonal prism plus two panels.
satellite IRIDIUM 153 Date of exalting 23.12.2017y. Average height of ISS IRIDIUM 153 hundred 789.87 km. Average velocity IRIDIUM 153 is 26856.98 km/h. Inclination IRIDIUM 153 satellite 86.4°.TLE
Average velocity IRIDIUM 153
Average inclination IRIDIUM 153
Mean right ascension of the ascending node (RAAN) IRIDIUM 153
Mean argument of perigee IRIDIUM 153
Mean semi-major axis of the orbit IRIDIUM 153
Mean orbital eccentricity IRIDIUM 153
ISS
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