ASCENT
Informationen über den Satelliten. ASCENT
| Name im Katalog Spacetrack | ASCENT |
| Folge ASCENT | ASCENT Tracker |
| Flugzeiten ASCENT | Flugzeiten ASCENT |
| In die Umlaufbahn bringen |
2021-12-07 (3 vor Jahren)
|
| Tage im Orbit | 1266 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perygeum | 35511 km |
| Apogäum | 35527 km |
| Neigung der Umlaufbahn (Inklination) | 3.18° |
| Runden pro Tag | 1 |
| Höhe ASCENT | 35515.96 km |
Informationen über ASCENT
Demonstrate various CubeSat operations in geostationary orbit (GEO). AFRL will provide and integrate the ASCENT payload.\r\nBlue Canyon provided the 12U CubeSat bus, avionics, flight software, Guidance Navigation and Control actuators and sensors, batteries, solar panels, solar array drives, two propulsion systems, and RF communication hardware. BCT was on-site during commissioning and ensured the spacecraft was in a safe, stable power and thermal attitude before releasing operations to the lab to complete the mission objectives.\r\nThe Ascent mission is evaluating the performance of commercial-off-the-shelf technology and capabilities in the GEO space environment, only previously seen in LEO flight experiments. Ascent comprises several demonstrations that include flying two propulsion systems and the first GEO application of the Georgia Tech cold gas propulsion system to provide momentum management. BCT contacted the spacecraft on the first acquisition and continues to support on-orbit questions as needed.
der Satellit ASCENT hinausgetragen 07.12.2021r. Durchschnittshöhe ASCENT Text Nummer 1: das. 35515.96 km. Durchschnittsgeschwindigkeit ASCENT beträgt 11104.61 km/h. Neigung ASCENT Satelliten 2.68°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. ASCENT
Durchschnittsgeschwindigkeit ASCENT
Durchschnitt ASCENT
