BS-3B (YURI 3B)
Satellite information BS-3B (YURI 3B) - YURI-3B (BS-3B)
| Spacetrack Directory Name | BS-3B (YURI 3B) |
| Alternative name | YURI-3B (BS-3B) |
| Follow BS-3B (YURI 3B) | BS-3B (YURI 3B) Tracker |
| Pass predictions BS-3B (YURI 3B) | Pass predictions BS-3B (YURI 3B) |
| Orbit launches |
1991-08-25 (35 years ago)
|
| Days in orbit | 12794 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 36193 km |
| Apogee | 36221 km |
| Orbit slope (inclination) | 13.4° |
| Laps per day | 1 |
| Height BS-3B (YURI 3B) | 36206.42 km |
Additional information BS-3B (YURI 3B)
BS-3B (YURI 3B), 21668 is a Japanese payload satellite in GEO that was launched on Sun, 25 Aug 1991 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-3B (YURI 3B) Date of exalting 25.08.1991y. Average height of ISS BS-3B (YURI 3B) hundred 36206.42 km. Average velocity BS-3B (YURI 3B) is 11014.3 km/h. Inclination BS-3B (YURI 3B) satellite 13.4°.TLE
Average velocity BS-3B (YURI 3B)
Average inclination BS-3B (YURI 3B)
Mean right ascension of the ascending node (RAAN) BS-3B (YURI 3B)
Mean argument of perigee BS-3B (YURI 3B)
Mean semi-major axis of the orbit BS-3B (YURI 3B)
Mean orbital eccentricity BS-3B (YURI 3B)
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