IRIDIUM 169
Satellite information IRIDIUM 169 - Iridium Next SV169
| Spacetrack Directory Name | IRIDIUM 169 |
| Alternative name | Iridium Next SV169 |
| Group | IRIDIUM |
| Follow IRIDIUM 169 | IRIDIUM 169 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 169 | Pass predictions IRIDIUM 169 |
| 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 | 758 km |
| Apogee | 768 km |
| Orbit slope (inclination) | 86.43° |
| Laps per day | 14 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 169 | 775.3 km |
Additional information IRIDIUM 169
IRIDIUM 169 (also known as Iridium Next SV169) is a communication and traffic monitoring satellite operated by IRIDS. It was launched on January 11, 2019, from the AFWTR Launch Site at SLC4E using a Falcon 9 launch vehicle. The satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters. Its dry mass is 700 kg, with a launch mass of 860 kg. It is equipped with an L-band payload, Ka-band cross-links and downlinks, and an ADS-B payload (part of the configuration on 58 satellites). IRIDIUM 169s power comes from two deployable solar arrays and batteries. The satellites shape is described as a half hex prism with two panels, and it has been designed for a 10-year lifetime with plans for a 15-year operational span.
satellite IRIDIUM 169 Date of exalting 11.01.2019y. Average height of ISS IRIDIUM 169 hundred 775.3 km. Average velocity IRIDIUM 169 is 26884.32 km/h. Inclination IRIDIUM 169 satellite 86.42°.TLE
Average velocity IRIDIUM 169
Average inclination IRIDIUM 169
Mean right ascension of the ascending node (RAAN) IRIDIUM 169
Mean argument of perigee IRIDIUM 169
Mean semi-major axis of the orbit IRIDIUM 169
Mean orbital eccentricity IRIDIUM 169
ISS
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