JCSAT 2
Satellite information JCSAT 2
| Spacetrack Directory Name | JCSAT 2 |
| Follow JCSAT 2 | JCSAT 2 Tracker |
| Pass predictions JCSAT 2 | Pass predictions JCSAT 2 |
| Orbit launches |
1990-01-01 (36 years ago)
|
| Days in orbit | 13399 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Perigee | 36018 km |
| Apogee | 36542 km |
| Orbit slope (inclination) | 16.02° |
| Laps per day | 1 |
| Height JCSAT 2 | 36280.31 km |
Additional information JCSAT 2
JCSAT 2, 20402 is a payload satellite owned by JCSAT (JP) in GEO that was launched on Mon, 01 Jan 1990 UTC via a COMMERCIAL TITAN 3 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 2 Date of exalting 01.01.1990y. Average height of ISS JCSAT 2 hundred 36280.31 km. Average velocity JCSAT 2 is 11004.79 km/h. Inclination JCSAT 2 satellite 16.01°.TLE
Average velocity JCSAT 2
Average inclination JCSAT 2
Mean right ascension of the ascending node (RAAN) JCSAT 2
Mean argument of perigee JCSAT 2
Mean semi-major axis of the orbit JCSAT 2
Mean orbital eccentricity JCSAT 2
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