FLOCK 4BE 24
Satellite information FLOCK 4BE 24 - 2024-149AP
| Spacetrack Directory Name | FLOCK 4BE 24 |
| Alternative name | 2024-149AP |
| Follow FLOCK 4BE 24 | FLOCK 4BE 24 Tracker |
| Pass predictions FLOCK 4BE 24 | Pass predictions FLOCK 4BE 24 |
| Orbit launches |
2024-08-16 (2 years ago)
|
| Days in orbit | 733 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 506 km |
| Apogee | 516 km |
| Orbit slope (inclination) | 97.37° |
| Laps per day | 15 |
| Height FLOCK 4BE 24 | 463.99 km |
Additional information FLOCK 4BE 24
FLOCK 4BE 24, 60505 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 24 Date of exalting 16.08.2024y. Average height of ISS FLOCK 4BE 24 hundred 463.99 km. Average velocity FLOCK 4BE 24 is 27489.36 km/h. Inclination FLOCK 4BE 24 satellite 97.38°.TLE
Average velocity FLOCK 4BE 24
Average inclination FLOCK 4BE 24
Mean right ascension of the ascending node (RAAN) FLOCK 4BE 24
Mean argument of perigee FLOCK 4BE 24
Mean semi-major axis of the orbit FLOCK 4BE 24
Mean orbital eccentricity FLOCK 4BE 24
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