Norad Identifikationsnummer: 49261
| Name im Katalog Spacetrack | OBJECT B |
| Folge OBJECT B | OBJECT B Tracker |
| Flugzeiten OBJECT B | Flugzeiten OBJECT B |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 1783 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | hier |
| Neigung der Umlaufbahn (Inklination) | 97.37° |
| Runden pro Tag | 15 |
| Höhe OBJECT B | 485.74 km |
Cesium Satellite 1 and 2 are 6U CubeSats with Cesium Nightingale 1 active phased array and inter-satellite link payloads. The spacecrafts have a high-accuracy attitude system with a star tracker and a state-of-the-art electric propulsion system.\r\nDemonstrate proprietary hardware and software in addition to testing intersatellite links and Ka-band communications.\r\nOnce the cubesats are in orbit, Cesium plans to demonstrate the performance of its Ka-band active phased array, software-defined radio and single-board computer, a device about the size of a credit card. In addition, the firm plans to conduct on-orbit experiments.\r\nCesium is offering customers the ability to purchase time on the five-year Cesium Mission 1 to experiment with active phased array and intersatellite links. Customers have expressed interest, for example, in testing waveform switching, edge processing and communications link optimization
der Satellit OBJECT B hinausgetragen 27.09.2021r. Durchschnittshöhe OBJECT B Text Nummer 1: das. 485.74 km. Durchschnittsgeschwindigkeit OBJECT B beträgt 27445.75 km/h. Neigung OBJECT B Satelliten 97.39°.