| Names | JCSAT-6 (order to Feb 1999) JCSAT-4A (Feb 1999 onward) |
|---|---|
| Mission type | Communications |
| Operator | SKY Perfect JSAT Group |
| COSPAR ID | 1999-006A |
| SATCAT no. | 25630 |
| Mission duration | 14.5 years (planned) 25 years, 8 months and 29 days (elasped) |
| Spacecraft properties | |
| Spacecraft | JCSAT-6 |
| Spacecraft type | JCSAT |
| Bus | HS-601 |
| Manufacturer | Hughes |
| Launch mass | 2,900 kilograms (6,400 lb) |
| Start of mission | |
| Launch date | 16 February 1999, 01:45:26 UTC |
| Rocket | Atlas IIAS (AC-152) |
| Launch site | Cape Canaveral, LC-36A |
| Contractor | International Launch Services (ILS) |
| Orbital parameters | |
| Reference system | Geocentric orbit |
| Regime | Geostationary orbit |
| Longitude | 124° East |
| Transponders | |
| Band | 32 Ku band |
| Coverage area | Japan |
JCSAT-4A, designated JCSAT-6 before launch, is a Japanese geostationary communications satellite which is operated by JSAT Corporation (now SKY Perfect JSAT Group). It is positioned in geostationary orbit at a longitude of 124° East, from where it is used to provide broadcasting and corporate network communications to Japan.[1]
- ^ "JCSAT-4A". Sky Perfect JSAT. Archived from the original on 13 July 2009. Retrieved 8 August 2009.