YOTSUBA-KULOVER
Satellite information YOTSUBA-KULOVER
| Spacetrack Directory Name | YOTSUBA-KULOVER |
| Orbit launches |
1998-11-20 |
| Deorbitation |
|
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 414 km |
| Apogee | 418 km |
| Height YOTSUBA-KULOVER | 346.55 km |
Additional information YOTSUBA-KULOVER
YOTSUBA-KULOVER, 65941 is an ISS payload satellite in LEO that was delivered to the ISS. Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite YOTSUBA-KULOVER Date of exalting 20.11.1998y. Average height of ISS YOTSUBA-KULOVER hundred 346.55 km. Average velocity YOTSUBA-KULOVER is 27732.76 km/h. Inclination YOTSUBA-KULOVER satellite 51.62°.Average velocity YOTSUBA-KULOVER
Average inclination YOTSUBA-KULOVER
Mean right ascension of the ascending node (RAAN) YOTSUBA-KULOVER
Mean argument of perigee YOTSUBA-KULOVER
Mean semi-major axis of the orbit YOTSUBA-KULOVER
Mean orbital eccentricity YOTSUBA-KULOVER
ISS
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