LEMUR 2 JOHNNYTRUONG
Satellite information LEMUR 2 JOHNNYTRUONG - 2024-043BA
| Spacetrack Directory Name | LEMUR 2 JOHNNYTRUONG |
| Alternative name | 2024-043BA |
| Follow LEMUR 2 JOHNNYTRUONG | LEMUR 2 JOHNNYTRUONG Tracker |
| Pass predictions LEMUR 2 JOHNNYTRUONG | Pass predictions LEMUR 2 JOHNNYTRUONG |
| Orbit launches |
2024-03-04 (2 years ago)
|
| Days in orbit | 847 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 506 km |
| Apogee | 519 km |
| Orbit slope (inclination) | 97.54° |
| Laps per day | 16 |
| Height LEMUR 2 JOHNNYTRUONG | 433.5 km |
Additional information LEMUR 2 JOHNNYTRUONG
LEMUR 2 JOHNNYTRUONG, 59146 is an American payload satellite in SSO that was launched on Mon, 04 Mar 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 LEMUR 2 JOHNNYTRUONG Date of exalting 04.03.2024y. Average height of ISS LEMUR 2 JOHNNYTRUONG hundred 433.5 km. Average velocity LEMUR 2 JOHNNYTRUONG is 27550.9 km/h. Inclination LEMUR 2 JOHNNYTRUONG satellite 97.52°.TLE
Average orbit height LEMUR 2 JOHNNYTRUONG
Average velocity LEMUR 2 JOHNNYTRUONG
Average inclination LEMUR 2 JOHNNYTRUONG
ISS
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