JCSAT 3
Satellite information JCSAT 3
| Spacetrack Directory Name | JCSAT 3 |
| Follow JCSAT 3 | JCSAT 3 Tracker |
| Pass predictions JCSAT 3 | Pass predictions JCSAT 3 |
| Orbit launches |
1995-08-29 (31 years ago)
|
| Days in orbit | 11332 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36040 km |
| Apogee | 36168 km |
| Orbit slope (inclination) | 13.02° |
| Laps per day | 1 |
| Height JCSAT 3 | 36105.13 km |
Additional information JCSAT 3
JCSAT 3, 23649 is a payload satellite owned by JSAT (JP) in GEO that was launched on Tue, 29 Aug 1995 UTC via an ATLAS IIAS 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 3 Date of exalting 29.08.1995y. Average height of ISS JCSAT 3 hundred 36105.13 km. Average velocity JCSAT 3 is 11027.37 km/h. Inclination JCSAT 3 satellite 13.01°.TLE
Average velocity JCSAT 3
Average inclination JCSAT 3
Mean right ascension of the ascending node (RAAN) JCSAT 3
Mean argument of perigee JCSAT 3
Mean semi-major axis of the orbit JCSAT 3
Mean orbital eccentricity JCSAT 3
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