LEMUR 2 DEVERILL-M-T
Informationen über den Satelliten. LEMUR 2 DEVERILL-M-T - 2023-100F
| Name im Katalog Spacetrack | LEMUR 2 DEVERILL-M-T |
| Alternative Bezeichnung | 2023-100F |
| Folge LEMUR 2 DEVERILL-M-T | LEMUR 2 DEVERILL-M-T Tracker |
| Flugzeiten LEMUR 2 DEVERILL-M-T | Flugzeiten LEMUR 2 DEVERILL-M-T |
| In die Umlaufbahn bringen |
2023-07-18 (vor einem Jahr)
|
| Tage im Orbit | 677 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | RLLB (Rocket Lab Launch Base) |
| WWW | hier |
| Perygeum | 561 km |
| Apogäum | 584 km |
| Neigung der Umlaufbahn (Inklination) | 99.44° |
| Runden pro Tag | 15 |
| Höhe LEMUR 2 DEVERILL-M-T | 548.07 km |
Informationen über LEMUR 2 DEVERILL-M-T
LEMUR 2 DEVERILL-M-T, 57391 is a payload satellite owned by Spire (US) in SSO that was launched on Tue, 18 Jul 2023 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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.
der Satellit LEMUR 2 DEVERILL-M-T hinausgetragen 18.07.2023r. Durchschnittshöhe LEMUR 2 DEVERILL-M-T Text Nummer 1: das. 548.07 km. Durchschnittsgeschwindigkeit LEMUR 2 DEVERILL-M-T beträgt 27322.04 km/h. Neigung LEMUR 2 DEVERILL-M-T Satelliten 99.45°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. LEMUR 2 DEVERILL-M-T
Durchschnittsgeschwindigkeit LEMUR 2 DEVERILL-M-T
Durchschnitt LEMUR 2 DEVERILL-M-T
