| Name of Satellite, Alternate Names | Ardusat-1 |
| Country of Operator/Owner | USA |
| Operator/Owner | NanoSatisfi Inc. |
| Users | Commercial |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | Sun-Synchronous |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 410 |
| Apogee (km) | 415 |
| Eccentricity | 0.000189771325552709 |
| Inclination (degrees) | 51.65 |
| Period (minutes) | 92.81 |
| Launch Mass (kg.) | 1 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 19-11-2013 |
| Expected Lifetime | .25 yrs. |
| Contractor | NanoSatisfi, Inc. |
| Country of Contractor | USA |
| Launch Site | ISS |
| Launch Vehicle | JSSOD |
| COSPAR Number | 1998-067DA |
| NORAD Number | 39412 |
| Comments | Built around an Arduino processor and a set of sensors that can be programmed by students to conduct experiments. Goal is to "democratize access to space." |