JCSAT 2B
Satellite information JCSAT 2B
| Spacetrack Directory Name | JCSAT 2B |
| Follow JCSAT 2B | JCSAT 2B Tracker |
| Pass predictions JCSAT 2B | Pass predictions JCSAT 2B |
| Orbit launches |
2016-05-06 (10 years ago)
|
| Days in orbit | 3762 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Categories | |
| Perigee | 35778 km |
| Apogee | 35796 km |
| Orbit slope (inclination) | 0° |
| Laps per day | 1 |
| Orbit | GEO |
| Height JCSAT 2B | 35786.48 km |
Additional information JCSAT 2B
JCSAT 2B, 41471 is a payload satellite owned by Sky Perfect JSAT (JP) in GEO that was launched on Fri, 06 May 2016 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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 JCSAT 2B Date of exalting 06.05.2016y. Average height of ISS JCSAT 2B hundred 35786.48 km. Average velocity JCSAT 2B is 11068.93 km/h. Inclination JCSAT 2B satellite 0.02°.TLE
Average velocity JCSAT 2B
Average inclination JCSAT 2B
Mean right ascension of the ascending node (RAAN) JCSAT 2B
Mean argument of perigee JCSAT 2B
Mean semi-major axis of the orbit JCSAT 2B
Mean orbital eccentricity JCSAT 2B
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