FLOCK 4BE 26
Satellite information FLOCK 4BE 26 - 2024-149S
| Spacetrack Directory Name | FLOCK 4BE 26 |
| Alternative name | 2024-149S |
| Follow FLOCK 4BE 26 | FLOCK 4BE 26 Tracker |
| Pass predictions FLOCK 4BE 26 | Pass predictions FLOCK 4BE 26 |
| 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 | 508 km |
| Apogee | 517 km |
| Orbit slope (inclination) | 97.35° |
| Laps per day | 16 |
| Height FLOCK 4BE 26 | 431.89 km |
Additional information FLOCK 4BE 26
FLOCK 4BE 26, 60484 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 26 Date of exalting 16.08.2024y. Average height of ISS FLOCK 4BE 26 hundred 431.89 km. Average velocity FLOCK 4BE 26 is 27554.87 km/h. Inclination FLOCK 4BE 26 satellite 97.38°.TLE
Average velocity FLOCK 4BE 26
Average inclination FLOCK 4BE 26
Mean right ascension of the ascending node (RAAN) FLOCK 4BE 26
Mean argument of perigee FLOCK 4BE 26
Mean semi-major axis of the orbit FLOCK 4BE 26
Mean orbital eccentricity FLOCK 4BE 26
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