GENESIS 2
Informationen über den Satelliten. GENESIS 2
| Name im Katalog Spacetrack | GENESIS 2 |
| Folge GENESIS 2 | GENESIS 2 Tracker |
| Flugzeiten GENESIS 2 | Flugzeiten GENESIS 2 |
| In die Umlaufbahn bringen |
2007-06-28 (17 vor Jahren)
|
| Tage im Orbit | 6540 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | DLS (Dombarovsky Air Base, Russia) |
| Kategorie | |
| Perygeum | 490 km |
| Apogäum | 532 km |
| Neigung der Umlaufbahn (Inklination) | 64.47° |
| Runden pro Tag | 16 |
| Orbit | LEO (Nicht-polar geneigt) |
| Höhe GENESIS 2 | 429.49 km |
Informationen über GENESIS 2
Genesis II is the second experimental space habitat designed and built by the private American firm Bigelow Aerospace, launched in 2007. As the second module sent into orbit by the company, this spacecraft builds on the data and experience gleaned from its previously orbited sister-ship Genesis I. Like its sister-ship and other modules being designed by Bigelow Aerospace, this spacecraft is based on the NASA TransHab design, which provides increased interior volume and reduced launch diameter along with potentially reduced mass compared to traditional rigid structures.
Genesis II was "retired" when its avionics systems stopped working after two and a half years. It remains in orbit, allowing researchers to continue testing the long-term viability of expandable space structures.
Orbital Elemente
Durchschnittshöhe der Orbitalbahn. GENESIS 2
Durchschnittsgeschwindigkeit GENESIS 2
Durchschnitt GENESIS 2
Frequenzen GENESIS 2
W tabelce, częstotliwości. GENESIS 2.
