SEMI-1P
Satellite information SEMI-1P - Satelita
| Spacetrack Directory Name | SEMI-1P |
| Alternative name | Satelita |
| Follow SEMI-1P | SEMI-1P Tracker |
| Pass predictions SEMI-1P | Pass predictions SEMI-1P |
| Country/organisation of origin | Turcja (TURK) |
| Starting point | |
| Perigee | 493 km |
| Apogee | 507 km |
| Orbit slope (inclination) | 45.4° |
| Laps per day | 15 |
| Height SEMI-1P | 508.51 km |
Additional information SEMI-1P
OBJECT F, 66298 is a satellite in LEO that was launched on Sun, 02 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.
Average height of ISS SEMI-1P hundred 508.51 km. Average velocity SEMI-1P is 27403.86 km/h. Inclination SEMI-1P satellite 45.39°.TLE
Average velocity SEMI-1P
Average inclination SEMI-1P
Mean right ascension of the ascending node (RAAN) SEMI-1P
Mean argument of perigee SEMI-1P
Mean semi-major axis of the orbit SEMI-1P
Mean orbital eccentricity SEMI-1P
ISS
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