LEMUR 2 ALISIA
Satellite information LEMUR 2 ALISIA - 2025-009DB
| Spacetrack Directory Name | LEMUR 2 ALISIA |
| Alternative name | 2025-009DB |
| Follow LEMUR 2 ALISIA | LEMUR 2 ALISIA Tracker |
| Pass predictions LEMUR 2 ALISIA | Pass predictions LEMUR 2 ALISIA |
| Orbit launches |
2025-01-14 (one year ago)
|
| Days in orbit | 581 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 588 km |
| Apogee | 590 km |
| Orbit slope (inclination) | 97.69° |
| Laps per day | 15 |
| Height LEMUR 2 ALISIA | 577.5 km |
Additional information LEMUR 2 ALISIA
LEMUR 2 ALISIA, 62706 is a payload satellite owned by Spire (US) in SSO that was launched on Tue, 14 Jan 2025 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 ALISIA Date of exalting 14.01.2025y. Average height of ISS LEMUR 2 ALISIA hundred 577.5 km. Average velocity LEMUR 2 ALISIA is 27264.08 km/h. Inclination LEMUR 2 ALISIA satellite 97.71°.TLE
Average velocity LEMUR 2 ALISIA
Average inclination LEMUR 2 ALISIA
Mean right ascension of the ascending node (RAAN) LEMUR 2 ALISIA
Mean argument of perigee LEMUR 2 ALISIA
Mean semi-major axis of the orbit LEMUR 2 ALISIA
Mean orbital eccentricity LEMUR 2 ALISIA
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