About Communication Satellite "Sakura" (CS)
|
The Communication Satellites Sakura(CS) was used to conduct a variety of communications experiments aimed at actualizing practical satellite communications systems in Japan. |
|---|
Major Characteristics
Sakura (CS)
| Launch Date | 12/15/1977 |
|---|---|
| Launch Vehicle | Delta 2914 Launch Vehicle (U.S.) |
| Launch Site | Kennedy Space Center |
| Orbit | Geostationary/135deg. E. longitude |
| Weight | 350kg |
Sakura-2a (CS-2a), Sakura-2b (CS-2b)
| Sakura-2a (CS-2a) |
Launch Date | 2/4/1983 |
|---|---|---|
| Launch Vehicle | N-II Launch Vehicle (N10F) | |
| Launch Site | Tanegashima Space Center | |
| Orbit | Geostationary/132deg. E. longitude | |
| Sakura-2b (CS-2b) |
Launch Date | 2/22/1980 |
| Launch Vehicle | N-II Launch Vehicle (N11F) | |
| Launch Site | Tanegashima Space Center | |
| Orbit | Geostationary/136deg. E. longitude | |
| Weight | 350kg | |
Sakura-3a (CS-3a), Sakura-3b (CS-3b)
| Sakura-3a (CS-3a) |
Launch Date | 2/19/1988 |
|---|---|---|
| Launch Vehicle | H-I Launch Vehicle (H18F) | |
| Launch Site | Tanegashima Space Center | |
| Orbit | Geostationary/132deg. E. longitude | |
| Sakura-3b (CS-3b) |
Launch Date | 9/16/1988 |
| Launch Vehicle | H-I Launch Vehicle (H19F) | |
| Launch Site | Tanegashima Space Center | |
| Orbit | Geostationary/136deg. E. longitude | |
| Weight | 550kg | |