LEMUR-2 GRAM-E-SUE
Informationen über den Satelliten. LEMUR-2 GRAM-E-SUE - TWILIGHT H
| Name im Katalog Spacetrack | LEMUR-2 GRAM-E-SUE |
| Alternative Bezeichnung | TWILIGHT H |
| Folge LEMUR-2 GRAM-E-SUE | LEMUR-2 GRAM-E-SUE Tracker |
| Flugzeiten LEMUR-2 GRAM-E-SUE | Flugzeiten LEMUR-2 GRAM-E-SUE |
| In die Umlaufbahn bringen |
2026-01-11 g.01:00 (2 Monate vor)
|
| Tage im Orbit | 70 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Perygeum | 599 km |
| Apogäum | 611 km |
| Neigung der Umlaufbahn (Inklination) | 97.8° |
| Runden pro Tag | 15 |
| Höhe LEMUR-2 GRAM-E-SUE | 617.6 km |
Informationen über LEMUR-2 GRAM-E-SUE
OBJECT H, 67370 is a satellite in SSO that was launched on Sun, 11 Jan 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.
der Satellit LEMUR-2 GRAM-E-SUE hinausgetragen 11.01.2026r. Durchschnittshöhe LEMUR-2 GRAM-E-SUE Text Nummer 1: das. 617.6 km. Durchschnittsgeschwindigkeit LEMUR-2 GRAM-E-SUE beträgt 27185.54 km/h. Neigung LEMUR-2 GRAM-E-SUE Satelliten 97.8°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. LEMUR-2 GRAM-E-SUE
Durchschnittsgeschwindigkeit LEMUR-2 GRAM-E-SUE
Durchschnitt LEMUR-2 GRAM-E-SUE
Frequenzen LEMUR-2 GRAM-E-SUE
W tabelce, częstotliwości. LEMUR-2 GRAM-E-SUE.
| Downlink | Modus |
|---|---|
| 401.100 MHz | BPSK |
| 401.100 MHz | BPSK |
