BS-2B (YURI 2B)
Satellite information BS-2B (YURI 2B) - YURI-2B (BS-2B)
| Spacetrack Directory Name | BS-2B (YURI 2B) |
| Alternative name | YURI-2B (BS-2B) |
| Follow BS-2B (YURI 2B) | BS-2B (YURI 2B) Tracker |
| Pass predictions BS-2B (YURI 2B) | Pass predictions BS-2B (YURI 2B) |
| Orbit launches |
1986-02-12 (40 years ago)
|
| Days in orbit | 14814 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 36017 km |
| Apogee | 36112 km |
| Orbit slope (inclination) | 12.18° |
| Laps per day | 1 |
| Height BS-2B (YURI 2B) | 36063.06 km |
Additional information BS-2B (YURI 2B)
BS-2B (YURI 2B), 16597 is a payload satellite owned by NASDA (JP) in GEO that was launched on Wed, 12 Feb 1986 UTC via an N-2 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-2B (YURI 2B) Date of exalting 12.02.1986y. Average height of ISS BS-2B (YURI 2B) hundred 36063.06 km. Average velocity BS-2B (YURI 2B) is 11032.86 km/h. Inclination BS-2B (YURI 2B) satellite 12.19°.TLE
Average velocity BS-2B (YURI 2B)
Average inclination BS-2B (YURI 2B)
Mean right ascension of the ascending node (RAAN) BS-2B (YURI 2B)
Mean argument of perigee BS-2B (YURI 2B)
Mean semi-major axis of the orbit BS-2B (YURI 2B)
Mean orbital eccentricity BS-2B (YURI 2B)
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