FLOCK 4BE 2
Satellite information FLOCK 4BE 2 - 2024-149AV
| Spacetrack Directory Name | FLOCK 4BE 2 |
| Alternative name | 2024-149AV |
| Follow FLOCK 4BE 2 | FLOCK 4BE 2 Tracker |
| Pass predictions FLOCK 4BE 2 | Pass predictions FLOCK 4BE 2 |
| Orbit launches |
2024-08-16 (2 years ago)
|
| Days in orbit | 783 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 506 km |
| Apogee | 514 km |
| Orbit slope (inclination) | 97.38° |
| Laps per day | 16 |
| Height FLOCK 4BE 2 | 436.35 km |
Additional information FLOCK 4BE 2
FLOCK 4BE 2, 60511 is a payload satellite owned by Planet (US) in SSO that was launched on Fri, 16 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite FLOCK 4BE 2 Date of exalting 16.08.2024y. Average height of ISS FLOCK 4BE 2 hundred 436.35 km. Average velocity FLOCK 4BE 2 is 27545.22 km/h. Inclination FLOCK 4BE 2 satellite 97.39°.TLE
Average velocity FLOCK 4BE 2
Average inclination FLOCK 4BE 2
Mean right ascension of the ascending node (RAAN) FLOCK 4BE 2
Mean argument of perigee FLOCK 4BE 2
Mean semi-major axis of the orbit FLOCK 4BE 2
Mean orbital eccentricity FLOCK 4BE 2
ISS
Buy us a coffee!
