HODOYOSHI 3
Informationen über den Satelliten. HODOYOSHI 3
| Name im Katalog Spacetrack | HODOYOSHI 3 |
| Folge HODOYOSHI 3 | HODOYOSHI 3 Tracker |
| Flugzeiten HODOYOSHI 3 | Flugzeiten HODOYOSHI 3 |
| In die Umlaufbahn bringen |
2014-06-19 g.02:00 (11 vor Jahren)
|
| Tage im Orbit | 4190 |
| Herkunftsland/-organisation | Japonia (JPN) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | DLS (Dombarovsky Air Base, Russia) |
| WWW | hier |
| Kategorie | |
| Perygeum | 607 km |
| Apogäum | 660 km |
| Neigung der Umlaufbahn (Inklination) | 97.62° |
| Runden pro Tag | 15 |
| Orbit | LEO (Sonnenbahn-synchron) |
| Höhe HODOYOSHI 3 | 631.04 km |
Informationen über HODOYOSHI 3
Hodoyoshi-3 is a Japanese micro-satellite launched in 2014. The satellite is built in 0.5x0.5x0.65m box-shape bus, optimized for piggy-back launch.
All instruments are powered by solar cells mounted on the spacecraft body and two stub wings, with estimated electrical power of 50W. For orbit-keeping, a hydrogen peroxide thruster is used. The latest information is available on FACEBOOK page. The satellite was developed under the Funding Program for World-Leading Innovation R&D on Science and Technology.
Orbital Elemente
Durchschnittshöhe der Orbitalbahn. HODOYOSHI 3
Durchschnittsgeschwindigkeit HODOYOSHI 3
Durchschnitt HODOYOSHI 3
Frequenzen HODOYOSHI 3
W tabelce, częstotliwości. HODOYOSHI 3.
| Downlink | Modus |
|---|---|
| 2263.606 MHz | FM |
