JCSAT 2A
Satellite information JCSAT 2A
| Spacetrack Directory Name | JCSAT 2A |
| Follow JCSAT 2A | JCSAT 2A Tracker |
| Pass predictions JCSAT 2A | Pass predictions JCSAT 2A |
| Orbit launches |
2002-03-29 (24 years ago)
|
| Days in orbit | 8925 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| WWW | Here |
| Categories | |
| Perigee | 36105 km |
| Apogee | 36171 km |
| Orbit slope (inclination) | 8.49° |
| Laps per day | 1 |
| Orbit | GEO |
| Height JCSAT 2A | 36138.23 km |
Additional information JCSAT 2A
JCSAT-2A, known as JCSAT-8 before launch, is a geostationary communications satellite operated by SKY Perfect JSAT Group (JSAT) which was designed and manufactured by Boeing on the BSS-601 platform. It has Ku band and C band payload and was used to replace JCSAT-2 at the 154°East longitude. It covers Japan, East Asia, Australia and Hawaii.
satellite JCSAT 2A Date of exalting 29.03.2002y. Average height of ISS JCSAT 2A hundred 36138.23 km. Average velocity JCSAT 2A is 11023.09 km/h. Inclination JCSAT 2A satellite 8.46°.TLE
Average velocity JCSAT 2A
Average inclination JCSAT 2A
Mean right ascension of the ascending node (RAAN) JCSAT 2A
Mean argument of perigee JCSAT 2A
Mean semi-major axis of the orbit JCSAT 2A
Mean orbital eccentricity JCSAT 2A
ISS
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