JCSAT 16
Satellite information JCSAT 16
| Spacetrack Directory Name | JCSAT 16 |
| Follow JCSAT 16 | JCSAT 16 Tracker |
| Pass predictions JCSAT 16 | Pass predictions JCSAT 16 |
| Orbit launches |
2016-08-14 (10 years ago)
|
| Days in orbit | 3662 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Categories | |
| Perigee | 35785 km |
| Apogee | 35790 km |
| Orbit slope (inclination) | 0.01° |
| Laps per day | 1 |
| Orbit | GEO |
| Height JCSAT 16 | 35786.51 km |
Additional information JCSAT 16
JCSAT 16, 41729 is a payload satellite owned by Sky Perfect JSAT (JP) in GEO that was launched on Sun, 14 Aug 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 16 Date of exalting 14.08.2016y. Average height of ISS JCSAT 16 hundred 35786.51 km. Average velocity JCSAT 16 is 11068.93 km/h. Inclination JCSAT 16 satellite 0.02°.TLE
Average velocity JCSAT 16
Average inclination JCSAT 16
Mean right ascension of the ascending node (RAAN) JCSAT 16
Mean argument of perigee JCSAT 16
Mean semi-major axis of the orbit JCSAT 16
Mean orbital eccentricity JCSAT 16
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