NANOSAT 1B
Informationen über den Satelliten. NANOSAT 1B
| Name im Katalog Spacetrack | NANOSAT 1B |
| Folge NANOSAT 1B | NANOSAT 1B Tracker |
| Flugzeiten NANOSAT 1B | Flugzeiten NANOSAT 1B |
| In die Umlaufbahn bringen |
2009-07-29 (16 vor Jahren)
|
| Tage im Orbit | 6086 |
| Herkunftsland/-organisation | Hiszpania (SPN) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Kategorie | |
| Perygeum | 575 km |
| Apogäum | 656 km |
| Neigung der Umlaufbahn (Inklination) | 98.1° |
| Runden pro Tag | 15 |
| Orbit | LEO (Sonnenbahn-synchron) |
| Höhe NANOSAT 1B | 604.66 km |
Informationen über NANOSAT 1B
The Nanosat-1B Spanish satellite, designed, developed and operated by the Instituto Nacional de Técnica Aeroespacial (National Institute of Aerospace Technology), INTA, is a nano-satellite which weighs 22 kg. Its main mission is the communication between remote sites like the Antarctic, the Hespérides warship and Spain.
The Nanosat-1B has fourteen sides, all of them covered by solar panels but the bottom one where the following antennas are installed: a medium gain UHF four wire antenna and two patch antennas.
On the top side there are four UHF monopoles. The solar sensors and the Vectorsol experiment are located in the middle tray, being all the other equipment and experiments located inside the satellite.
The Nanosat-1B covers all the earth due to his polar orbit and it stores scientific data which are unloaded when the satellite passes the Control Centre vertical (located at INTA, Torrejón, Madrid) and the mobile stations (Nano-Terminals).
This satellite was launched on 29 July 2009 at 18:46 UTC from the ?Cosmodromo? in Baikonur (Kazajistan), launchpad 95 area 109, by a Dnepr rocket along with other five satellites: the DubaiSat-1 (this one being the main load), Deimos-1, UK-DMC 2, Aprizesat-3 and Aprizesat-4.
Orbital Elemente
Durchschnittshöhe der Orbitalbahn. NANOSAT 1B
Durchschnittsgeschwindigkeit NANOSAT 1B
Durchschnitt NANOSAT 1B
