ICEYE-X42
Informationen über den Satelliten. ICEYE-X42 - 2025-009CT
| Name im Katalog Spacetrack | ICEYE-X42 |
| Alternative Bezeichnung | 2025-009CT |
| Folge ICEYE-X42 | ICEYE-X42 Tracker |
| Flugzeiten ICEYE-X42 | Flugzeiten ICEYE-X42 |
| In die Umlaufbahn bringen |
2025-01-14 (4 Monate vor)
|
| Tage im Orbit | 135 |
| Herkunftsland/-organisation | Finland (FIN) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Perygeum | 591 km |
| Apogäum | 593 km |
| Neigung der Umlaufbahn (Inklination) | 97.74° |
| Runden pro Tag | 15 |
| Höhe ICEYE-X42 | 602.75 km |
Informationen über ICEYE-X42
ICEYE-X42, 62698 is a Finnish payload satellite in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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 ICEYE-X42 hinausgetragen 14.01.2025r. Durchschnittshöhe ICEYE-X42 Text Nummer 1: das. 602.75 km. Durchschnittsgeschwindigkeit ICEYE-X42 beträgt 27214.8 km/h. Neigung ICEYE-X42 Satelliten 97.74°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. ICEYE-X42
Durchschnittsgeschwindigkeit ICEYE-X42
Durchschnitt ICEYE-X42
