JCSAT 10
Satellite information JCSAT 10 - JCSAT-3A
| Spacetrack Directory Name | JCSAT 10 |
| Alternative name | JCSAT-3A |
| Follow JCSAT 10 | JCSAT 10 Tracker |
| Pass predictions JCSAT 10 | Pass predictions JCSAT 10 |
| Orbit launches |
2006-08-11 (20 years ago)
|
| Days in orbit | 7326 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Type | Satellite |
| Categories | |
| Perigee | 35775 km |
| Apogee | 35798 km |
| Orbit slope (inclination) | 0.05° |
| Laps per day | 1 |
| Orbit | GEO |
| Height JCSAT 10 | 35786.39 km |
Additional information JCSAT 10
JCSAT-3A, known as JCSAT-10 before launch, is a geostationary communications satellite operated by SKY Perfect JSAT Group (JSAT) which was designed and manufactured by Lockheed Martin on the A2100 platform.
satellite JCSAT 10 Date of exalting 11.08.2006y. Average height of ISS JCSAT 10 hundred 35786.39 km. Average velocity JCSAT 10 is 11068.94 km/h. Inclination JCSAT 10 satellite 0.02°.TLE
Average velocity JCSAT 10
Average inclination JCSAT 10
Mean right ascension of the ascending node (RAAN) JCSAT 10
Mean argument of perigee JCSAT 10
Mean semi-major axis of the orbit JCSAT 10
Mean orbital eccentricity JCSAT 10
ISS
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