2024-043BB - Norad ID: 59147
Spacetrack Directory Name | LEMUR 2 ROCINANTE |
Alternative name | 2024-043BB |
Follow LEMUR 2 ROCINANTE | LEMUR 2 ROCINANTE Tracker |
Pass predictions LEMUR 2 ROCINANTE | Pass predictions LEMUR 2 ROCINANTE |
Orbit launches |
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Days in orbit | 420 |
Country/organisation of origin | USA (US) |
Starting point | AFWTR (Vandenberg Air Force Base, USA) |
Perigee | 506 km |
Apogee | 519 km |
Orbit slope (inclination) | 97.5° |
Laps per day | 15 |
Height LEMUR 2 ROCINANTE | 498.39 km |
LEMUR 2 ROCINANTE, 59147 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 ROCINANTE Date of exalting 04.03.2024y. Average height of ISS LEMUR 2 ROCINANTE hundred 498.39 km. Average velocity LEMUR 2 ROCINANTE is 27420.55 km/h. Inclination LEMUR 2 ROCINANTE satellite 97.48°.
In the table below we show the frequencies LEMUR 2 ROCINANTE.
Downlink | Mode |
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2260.000 MHz | FM |