LEMUR-2-DEANANDMAEVE
Informationen über den Satelliten. LEMUR-2-DEANANDMAEVE - TRANSPORTER-15 N
| Name im Katalog Spacetrack | LEMUR-2-DEANANDMAEVE |
| Alternative Bezeichnung | TRANSPORTER-15 N |
| Folge LEMUR-2-DEANANDMAEVE | LEMUR-2-DEANANDMAEVE Tracker |
| Flugzeiten LEMUR-2-DEANANDMAEVE | Flugzeiten LEMUR-2-DEANANDMAEVE |
| In die Umlaufbahn bringen |
2025-11-28 (3 Monate vor)
|
| Tage im Orbit | 114 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Perygeum | 507 km |
| Apogäum | 515 km |
| Neigung der Umlaufbahn (Inklination) | 97.43° |
| Runden pro Tag | 15 |
| Höhe LEMUR-2-DEANANDMAEVE | 522.75 km |
Informationen über LEMUR-2-DEANANDMAEVE
OBJECT N, 66678 is a satellite in SSO that was launched on Fri, 28 Nov 2025 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.
der Satellit LEMUR-2-DEANANDMAEVE hinausgetragen 28.11.2025r. Durchschnittshöhe LEMUR-2-DEANANDMAEVE Text Nummer 1: das. 522.75 km. Durchschnittsgeschwindigkeit LEMUR-2-DEANANDMAEVE beträgt 27371.57 km/h. Neigung LEMUR-2-DEANANDMAEVE Satelliten 97.43°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. LEMUR-2-DEANANDMAEVE
Durchschnittsgeschwindigkeit LEMUR-2-DEANANDMAEVE
Durchschnitt LEMUR-2-DEANANDMAEVE
Frequenzen LEMUR-2-DEANANDMAEVE
W tabelce, częstotliwości. LEMUR-2-DEANANDMAEVE.
| Downlink | Modus |
|---|---|
| 401.025 MHz | 4k8_FSK |
| 401.025 MHz | GMSK |
