| Name of Satellite, Alternate Names | SOHLA 1 (Space Oriented Higashiosaka Leading Association, Maido 1) |
| Country of Operator/Owner | Japan |
| Operator/Owner | Astrotech SOHLA |
| Users | Civil |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | Sun-Synchronous |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 657 |
| Apogee (km) | 665 |
| Eccentricity | 0.000568909116768596 |
| Inclination (degrees) | 98.1 |
| Period (minutes) | 98 |
| Launch Mass (kg.) | 50 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 23-01-2009 |
| Expected Lifetime | |
| Contractor | Space Oriented Higashiosaka Leading Association |
| Country of Contractor | Japan |
| Launch Site | Tanegashima Space Center |
| Launch Vehicle | H-2A |
| COSPAR Number | 2009-002E |
| NORAD Number | 33496 |
| Comments | Observe lightening. |