HORYU 4
Satellite information HORYU 4 - HORYU-4
| Spacetrack Directory Name | HORYU 4 |
| Alternative name | HORYU-4 |
| Orbit launches |
2016-02-17 g.01:00 |
| Deorbitation |
|
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| WWW | Here |
| Categories | |
| Perigee | 552 km |
| Apogee | 571 km |
| Height HORYU 4 | 379.3 km |
Additional information HORYU 4
Horyu-4 is testing an experimental high-voltage solar array system and observing corresponding spacecraft charging effects on the satellite caused by the high voltage. The mission of Horyu-4 is to: acquire current waveform of arcing phenomena on high voltage solar array. Acquire image of arcing phenomena on high voltage solar array. Advance our knowledge on spacecraft charging. Contribute to reliability improvement of present space systems and realization of future high power space system.
satellite HORYU 4 Date of exalting 17.02.2016y. Average height of ISS HORYU 4 hundred 379.3 km. Average velocity HORYU 4 is 27668.04 km/h. Inclination HORYU 4 satellite 30.99°.Average velocity HORYU 4
Average inclination HORYU 4
Mean right ascension of the ascending node (RAAN) HORYU 4
Mean argument of perigee HORYU 4
Mean semi-major axis of the orbit HORYU 4
Mean orbital eccentricity HORYU 4
Photos HORYU 4 Photos: 1
ISS
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