SOCRATES
Informationen über den Satelliten. SOCRATES
| Name im Katalog Spacetrack | SOCRATES |
| Folge SOCRATES | SOCRATES Tracker |
| Flugzeiten SOCRATES | Flugzeiten SOCRATES |
| In die Umlaufbahn bringen |
2014-05-24 (11 vor Jahren)
|
| Tage im Orbit | 4023 |
| Herkunftsland/-organisation | Japonia (JPN) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | TANSC (Tanegashima Space Center, Japan) |
| WWW | hier |
| Kategorie | |
| Perygeum | 609 km |
| Apogäum | 621 km |
| Neigung der Umlaufbahn (Inklination) | 97.89° |
| Runden pro Tag | 15 |
| Orbit | LEO (Sonnenbahn-synchron) |
| Höhe SOCRATES | 608.16 km |
Informationen über SOCRATES
SOCRATES or Space Optical Communications Research Advanced Technology Satellite is a Japanese micro-satellite launched in 2014. The satellite is purely a technology demonstrator intended to help AES company to gain experience in basic mission control, attitude control and spacecraft communications. Its main experiment is SOTA (Small Optical TrAnsponder), an optical small satellite communications demonstrator.
All subsystems of spacecraft are powered by solar cells mounted on spacecraft body and stub wings, with estimated electrical power of 120W BOL degrading to 100W EOL.
Orbital Elemente
Durchschnittshöhe der Orbitalbahn. SOCRATES
Durchschnittsgeschwindigkeit SOCRATES
Durchschnitt SOCRATES
Frequenzen SOCRATES
W tabelce, częstotliwości. SOCRATES.
