| Name of Satellite, Alternate Names | KKS-1 (Kouku Kousen Satellite One, Kiseki) |
| Country of Operator/Owner | Japan |
| Operator/Owner | Tokyo Metropolitan College of Industrial Technology |
| Users | Civil |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 651 |
| Apogee (km) | 667 |
| Eccentricity | 0.00113814198321241 |
| Inclination (degrees) | 98.03 |
| Period (minutes) | 97.92 |
| Launch Mass (kg.) | 3 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 23-01-2009 |
| Expected Lifetime | 1 yr. |
| Contractor | Tokyo Metropolitan College of Industrial Technology |
| Country of Contractor | Japan |
| Launch Site | Tanegashima Space Center |
| Launch Vehicle | H-2A |
| COSPAR Number | 2009-002H |
| NORAD Number | 33499 |
| Comments | Experiments on micro-thrusters, basic experiments on 3-axis attitude control and take land images with a camera. |