BS-3A (YURI 3A)
Satellite information BS-3A (YURI 3A) - YURI-3A (BS-3A)
| Spacetrack Directory Name | BS-3A (YURI 3A) |
| Alternative name | YURI-3A (BS-3A) |
| Follow BS-3A (YURI 3A) | BS-3A (YURI 3A) Tracker |
| Pass predictions BS-3A (YURI 3A) | Pass predictions BS-3A (YURI 3A) |
| Orbit launches |
1990-08-28 (36 years ago)
|
| Days in orbit | 13156 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 36157 km |
| Apogee | 36245 km |
| Orbit slope (inclination) | 15.62° |
| Laps per day | 1 |
| Height BS-3A (YURI 3A) | 36201.42 km |
Additional information BS-3A (YURI 3A)
BS-3A (YURI 3A), 20771 is a Japanese payload satellite in GEO that was launched on Tue, 28 Aug 1990 UTC via an H-1 launch vehicle from the Tanegashima Space Center (TNSTA). Payloads include a variety of satellites, spacecraft, and rockets 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 BS-3A (YURI 3A) Date of exalting 28.08.1990y. Average height of ISS BS-3A (YURI 3A) hundred 36201.42 km. Average velocity BS-3A (YURI 3A) is 11014.86 km/h. Inclination BS-3A (YURI 3A) satellite 15.62°.TLE
Average velocity BS-3A (YURI 3A)
Average inclination BS-3A (YURI 3A)
Mean right ascension of the ascending node (RAAN) BS-3A (YURI 3A)
Mean argument of perigee BS-3A (YURI 3A)
Mean semi-major axis of the orbit BS-3A (YURI 3A)
Mean orbital eccentricity BS-3A (YURI 3A)
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