FLOCK 4BE 28
Satellite information FLOCK 4BE 28 - 2024-149BD
| Spacetrack Directory Name | FLOCK 4BE 28 |
| Alternative name | 2024-149BD |
| Follow FLOCK 4BE 28 | FLOCK 4BE 28 Tracker |
| Pass predictions FLOCK 4BE 28 | Pass predictions FLOCK 4BE 28 |
| 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 | 504 km |
| Apogee | 515 km |
| Orbit slope (inclination) | 97.37° |
| Laps per day | 15 |
| Height FLOCK 4BE 28 | 458.91 km |
Additional information FLOCK 4BE 28
FLOCK 4BE 28, 60519 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 28 Date of exalting 16.08.2024y. Average height of ISS FLOCK 4BE 28 hundred 458.91 km. Average velocity FLOCK 4BE 28 is 27499.58 km/h. Inclination FLOCK 4BE 28 satellite 97.38°.TLE
Average velocity FLOCK 4BE 28
Average inclination FLOCK 4BE 28
Mean right ascension of the ascending node (RAAN) FLOCK 4BE 28
Mean argument of perigee FLOCK 4BE 28
Mean semi-major axis of the orbit FLOCK 4BE 28
Mean orbital eccentricity FLOCK 4BE 28
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