IRIDIUM 158
Satellite information IRIDIUM 158 - Iridium Next SV158
| Spacetrack Directory Name | IRIDIUM 158 |
| Alternative name | Iridium Next SV158 |
| Group | IRIDIUM |
| Follow IRIDIUM 158 | IRIDIUM 158 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 158 | Pass predictions IRIDIUM 158 |
| Orbit launches |
2018-07-25 (8 years ago)
|
| Days in orbit | 2999 |
| 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 158 | 789.86 km |
Additional information IRIDIUM 158
IRIDIUM 158 (also known as Iridium Next SV158) is a communication and traffic monitoring satellite operated by IRIDS. It was launched on July 25, 2018, from AFWTR SLC4E using a Falcon 9 launch vehicle. The satellite measures 3.1 meters in length with a diameter of 1.5 meters and spans 9.4 meters when its solar arrays are deployed. Its dry mass is 700 kg, and it was launched with a total mass of 860 kg. Equipped with an L-band payload for communication, Ka-band cross-links, and downlinks, as well as ADS-B and AIS-receiver capabilities (shared among 58 satellites), IRIDIUM 158 is designed to operate for up to 10 years, though the mission plans aim for a 15-year lifetime. The satellite uses two deployable solar arrays and batteries for power. It was manufactured by NGISGA and has a half hex prism shape with two panels.
satellite IRIDIUM 158 Date of exalting 25.07.2018y. Average height of ISS IRIDIUM 158 hundred 789.86 km. Average velocity IRIDIUM 158 is 26856.99 km/h. Inclination IRIDIUM 158 satellite 86.4°.TLE
Average velocity IRIDIUM 158
Average inclination IRIDIUM 158
Mean right ascension of the ascending node (RAAN) IRIDIUM 158
Mean argument of perigee IRIDIUM 158
Mean semi-major axis of the orbit IRIDIUM 158
Mean orbital eccentricity IRIDIUM 158
ISS
Buy us a coffee!
