HSU-SAT1

53462
Numer w katalogu Spacetrack
1998-11-20
Wyniesienie na orbitę
2023-03-09
8875 dni na orbicie
378.73 km
Wysokość średnia
27665.68 km/h
Prędkość średnia


Informacje o satelicie HSU-SAT1 - 1998-067UB

Nazwa w katalogu Spacetrack HSU-SAT1
Alternatywna nazwa 1998-067UB
Wyniesienie na orbitę 1998-11-20
Data deorbitacji 2023-03-09
Dni na orbicie 8875
Kraj/organizacja pochodzenia Japonia (JPN)
Miejsce startu TYMSC (Baikonur Cosmodrome, Kazakhstan)
WWW Tutaj
Perygeum 409 km
Apogeum 419 km

Informacje o HSU-SAT1

The main purpose of satellite mission are\r\nA technology demonstration of Electrical Power Supply On Board Computer and other bus components. \r\n HSU-SAT1 performs three-axis attitude control by combining aerodynamic stabilization and magnetic torquers. \r\n The modulated infrared light emitted from our ground station is experimented as command transmission link. The command format conforms to the infrared remote-control system used in electrical appliances. \r\n Camera image is downlinked by Slow Scan Television. The camera takes a photograph of the Earth. Image pixel size is 320x240. The photograph taken is converted into analog SSTV?signal, transferred to Communication and sent by FM-SSTV downlink. \r\n A technology demonstration of gyro sensor and magnetic sensor which has not been confirmed its operation in space. \r\n HSU-SAT1 provides a demonstration that modulated infrared light emitted from a ground station can be used as a command transmission link. HSU-SAT1 also evaluates new technologies for electrical power supply, on board computing, and other satellite bus components.



Średnia wysokość orbity HSU-SAT1

Średnia prędkość HSU-SAT1

Średnia inklinacja HSU-SAT1

Data aktualizacji: 2023-04-13 14:50:05