LEMUR-2-ELEONORE
Satellite information LEMUR-2-ELEONORE
| Spacetrack Directory Name | LEMUR-2-ELEONORE |
| Follow LEMUR-2-ELEONORE | LEMUR-2-ELEONORE Tracker |
| Pass predictions LEMUR-2-ELEONORE | Pass predictions LEMUR-2-ELEONORE |
| Orbit launches |
2026-07-07 (one month ago)
|
| Days in orbit | 37 |
| Country/organisation of origin | Niemcy (GER) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 582 km |
| Apogee | 598 km |
| Orbit slope (inclination) | 97.75° |
| Laps per day | 15 |
| Height LEMUR-2-ELEONORE | 601.68 km |
Additional information LEMUR-2-ELEONORE
OBJECT BZ, 69940 is a satellite in SSO that was launched on Tue, 07 Jul 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Unknown objects in Earths orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earths gravity.
satellite LEMUR-2-ELEONORE Date of exalting 07.07.2026y. Average height of ISS LEMUR-2-ELEONORE hundred 601.68 km. Average velocity LEMUR-2-ELEONORE is 27216.82 km/h. Inclination LEMUR-2-ELEONORE satellite 97.75°.TLE
Average velocity LEMUR-2-ELEONORE
Average inclination LEMUR-2-ELEONORE
Mean right ascension of the ascending node (RAAN) LEMUR-2-ELEONORE
Mean argument of perigee LEMUR-2-ELEONORE
Mean semi-major axis of the orbit LEMUR-2-ELEONORE
Mean orbital eccentricity LEMUR-2-ELEONORE
ISS
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