HODOYOSHI 3
Satellite information HODOYOSHI 3
| Spacetrack Directory Name | HODOYOSHI 3 |
| Follow HODOYOSHI 3 | HODOYOSHI 3 Tracker |
| Pass predictions HODOYOSHI 3 | Pass predictions HODOYOSHI 3 |
| Orbit launches |
2014-06-19 g.02:00 (12 years ago)
|
| Days in orbit | 4451 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | DLS (Dombarovsky Air Base, Russia) |
| WWW | Here |
| Categories | |
| Perigee | 607 km |
| Apogee | 660 km |
| Orbit slope (inclination) | 97.65° |
| Laps per day | 15 |
| Orbit | LEO (Sun-Synchronous) |
| Height HODOYOSHI 3 | 625.62 km |
Additional information 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.
TLE
Average velocity HODOYOSHI 3
Average inclination HODOYOSHI 3
Mean right ascension of the ascending node (RAAN) HODOYOSHI 3
Mean argument of perigee HODOYOSHI 3
Mean semi-major axis of the orbit HODOYOSHI 3
Mean orbital eccentricity HODOYOSHI 3
Frequency HODOYOSHI 3
In the table below we show the frequencies HODOYOSHI 3.
| Downlink | Mode |
|---|---|
| 2263.606 MHz | FM |
ISS
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