TRANSPORTER-17 OBJECT AS
Informationen über den Satelliten. TRANSPORTER-17 OBJECT AS
| Name im Katalog Spacetrack | TRANSPORTER-17 OBJECT AS |
| Folge TRANSPORTER-17 OBJECT AS | TRANSPORTER-17 OBJECT AS Tracker |
| Flugzeiten TRANSPORTER-17 OBJECT AS | Flugzeiten TRANSPORTER-17 OBJECT AS |
| In die Umlaufbahn bringen |
2026-07-07 (2 Monate vor)
|
| Tage im Orbit | 75 |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Perygeum | 589 km |
| Apogäum | 598 km |
| Neigung der Umlaufbahn (Inklination) | 97.75° |
| Runden pro Tag | 15 |
| Höhe TRANSPORTER-17 OBJECT AS | 605.38 km |
Informationen über TRANSPORTER-17 OBJECT AS
OBJECT AS, 69909 is a satellite in SSO that was launched on Tue, 07 Jul 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 TRANSPORTER-17 OBJECT AS hinausgetragen 07.07.2026r. Durchschnittshöhe TRANSPORTER-17 OBJECT AS Text Nummer 1: das. 605.38 km. Durchschnittsgeschwindigkeit TRANSPORTER-17 OBJECT AS beträgt 27209.6 km/h. Neigung TRANSPORTER-17 OBJECT AS Satelliten 97.75°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. TRANSPORTER-17 OBJECT AS
Durchschnittsgeschwindigkeit TRANSPORTER-17 OBJECT AS
Durchschnitt TRANSPORTER-17 OBJECT AS
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) TRANSPORTER-17 OBJECT AS
Mittleres Argument des Perigäums TRANSPORTER-17 OBJECT AS
Mittlere große Halbachse der Umlaufbahn TRANSPORTER-17 OBJECT AS
Mittlere Bahnexzentrizität TRANSPORTER-17 OBJECT AS
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