VELOX-I - Norad Identifikationsnummer: 40057
| Name im Katalog Spacetrack | VELOX 1 |
| Alternative Bezeichnung | VELOX-I |
| Folge VELOX 1 | VELOX 1 Tracker |
| Flugzeiten VELOX 1 | Flugzeiten VELOX 1 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 4512 |
| Herkunftsland/-organisation | Singapur (SING) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | SRILR (Satish Dhawan Space Centre, India) |
| WWW | hier |
| Kategorie | |
| Perygeum | 629 km |
| Apogäum | 642 km |
| Neigung der Umlaufbahn (Inklination) | 98.24° |
| Runden pro Tag | 15 |
| Orbit | LEO (Sonnenbahn-synchron) |
| Höhe VELOX 1 | 583.05 km |
To launch the first Singapore?s nanosatellite VELOX-I, which is designed, built, and operated by students from different schools in the College of Engineering, NTU. To acquire images of Earth and transmit them back to ground station. A narrow angle camera with tele-optics is used to provide high-resolution images of Earth from LEO. To carry out experiments relevant to technology demonstration.Payloads include: a vision system, a dual-FOV sun sensor. To piggyback launch a picosatellite (VELOX-PIII) for intersatellite communication experiment. Optics extension system all use spring-loaded mechanisms for deployment after launch. Imaging system with extended optics for 20 m ground resolution, a quantum physics payload and an intersatellite communications payload.
der Satellit VELOX 1 hinausgetragen 30.06.2014r. Durchschnittshöhe VELOX 1 Text Nummer 1: das. 583.05 km. Durchschnittsgeschwindigkeit VELOX 1 beträgt 27253.22 km/h. Neigung VELOX 1 Satelliten 98.25°.
W tabelce, częstotliwości. VELOX 1.
| Downlink | Leuchtfeuer | Modus | Rufzeichen |
|---|---|---|---|
| 145.980 MHz | Beacon: 145.980 | 9k6 FSK CW | VELOXI |