JCSAT 1
Satellite information JCSAT 1
| Spacetrack Directory Name | JCSAT 1 |
| Follow JCSAT 1 | JCSAT 1 Tracker |
| Pass predictions JCSAT 1 | Pass predictions JCSAT 1 |
| Orbit launches |
1989-03-06 (37 years ago)
|
| Days in orbit | 13713 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 35979 km |
| Apogee | 36008 km |
| Orbit slope (inclination) | 14.82° |
| Laps per day | 1 |
| Height JCSAT 1 | 35995.36 km |
Additional information JCSAT 1
JCSAT 1, 19874 is a payload satellite owned by JCSAT (JP) in GEO that was launched on Mon, 06 Mar 1989 UTC via an ARIANE 44LP launch vehicle from the French Guiana (FRGUI). 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 1 Date of exalting 06.03.1989y. Average height of ISS JCSAT 1 hundred 35995.36 km. Average velocity JCSAT 1 is 11041.67 km/h. Inclination JCSAT 1 satellite 14.82°.TLE
Average velocity JCSAT 1
Average inclination JCSAT 1
Mean right ascension of the ascending node (RAAN) JCSAT 1
Mean argument of perigee JCSAT 1
Mean semi-major axis of the orbit JCSAT 1
Mean orbital eccentricity JCSAT 1
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