IRIDIUM 176
Satellite information IRIDIUM 176 - Iridium Next SV176
| Spacetrack Directory Name | IRIDIUM 176 |
| Alternative name | Iridium Next SV176 |
| Group | IRIDIUM |
| Follow IRIDIUM 176 | IRIDIUM 176 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 176 | Pass predictions IRIDIUM 176 |
| 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 | 652 km |
| Apogee | 656 km |
| Orbit slope (inclination) | 86.61° |
| Laps per day | 15 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 176 | 666.11 km |
Additional information IRIDIUM 176
IRIDIUM 176, also known as Iridium Next SV176, is a communication and traffic monitoring satellite launched on January 11, 2019, from Vandenberg Air Force Base (AFWTR) using Falcon 9 as the launch vehicle. It was manufactured by NGISGA and owned by IRIDS. The satellite measures 3.1 meters in length with a diameter of 1.5 meters and a span of 9.4 meters. It has a dry mass of 700 kg and a launch mass of 860 kg, featuring a configuration known as ELiTeBus-1000. Its equipment includes an L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receiver. The satellite is powered by two deployable solar arrays and batteries. It has a design lifetime of 10 years but plans are set for it to operate up to 15 years.
satellite IRIDIUM 176 Date of exalting 11.01.2019y. Average height of ISS IRIDIUM 176 hundred 666.11 km. Average velocity IRIDIUM 176 is 27091.91 km/h. Inclination IRIDIUM 176 satellite 86.61°.TLE
Average velocity IRIDIUM 176
Average inclination IRIDIUM 176
Mean right ascension of the ascending node (RAAN) IRIDIUM 176
Mean argument of perigee IRIDIUM 176
Mean semi-major axis of the orbit IRIDIUM 176
Mean orbital eccentricity IRIDIUM 176
ISS
Buy us a coffee!
