IRIDIUM 175
Satellite information IRIDIUM 175 - Iridium Next SV175
| Spacetrack Directory Name | IRIDIUM 175 |
| Alternative name | Iridium Next SV175 |
| Group | IRIDIUM |
| Follow IRIDIUM 175 | IRIDIUM 175 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 175 | Pass predictions IRIDIUM 175 |
| Orbit launches |
2019-01-11 (7 years ago)
|
| Days in orbit | 2829 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| WWW | Here |
| Categories | |
| Perigee | 653 km |
| Apogee | 655 km |
| Orbit slope (inclination) | 86.45° |
| Laps per day | 14 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 175 | 717.42 km |
Additional information IRIDIUM 175
IRIDIUM 175 (OBJECT_ID: 2019-002G), also known as Iridium Next SV175, is a communication and traffic monitoring satellite manufactured by NGISGA for the owner IRIDS. Launched on January 11, 2019, from AFWTR SLC4E using a Falcon 9 launch vehicle, it has a designed lifetime of 10 years with plans to extend it up to 15 years. The satellite measures 3.1 meters in length and 1.5 meters in diameter, with a span of 9.4 meters. It weighs approximately 700 kg dry mass and had an initial launch mass of 860 kg. Equipped with L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receiver (part of a network on 58 satellites), it is powered by two deployable solar arrays and batteries. Its configuration, identified as ELiTeBus-1000 under the BUS category EliteBus, includes a Half Hex Prism+2 pan shape for its design.
satellite IRIDIUM 175 Date of exalting 11.01.2019y. Average height of ISS IRIDIUM 175 hundred 717.42 km. Average velocity IRIDIUM 175 is 26994.19 km/h. Inclination IRIDIUM 175 satellite 86.32°.TLE
Average velocity IRIDIUM 175
Average inclination IRIDIUM 175
Mean right ascension of the ascending node (RAAN) IRIDIUM 175
Mean argument of perigee IRIDIUM 175
Mean semi-major axis of the orbit IRIDIUM 175
Mean orbital eccentricity IRIDIUM 175
ISS
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