| Name of Satellite, Alternate Names | Can-X6 (Canadian Advanced Nanospace experiment; NTS [Nanosatellite Tracking Ships]) |
| Country of Operator/Owner | Canada |
| Operator/Owner | University of Toronto Institute for Aerospace Studies/Com Development International Ltd. |
| Users | Civil/Commercial |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | Sun-Synchronous |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 611 |
| Apogee (km) | 631 |
| Eccentricity | 0.00143041052782148 |
| Inclination (degrees) | 97.8 |
| Period (minutes) | 97.1 |
| Launch Mass (kg.) | 16 |
| Dry Mass (kg.) | 6.5 |
| Power (watts) | |
| Date of Launch | 28-04-2008 |
| Expected Lifetime | .5 yrs. |
| Contractor | University of Toronto Institute for Aerospace Studies/Com Development International Ltd. |
| Country of Contractor | Canada |
| Launch Site | Sriharikota Launch Station |
| Launch Vehicle | PSLV C9 |
| COSPAR Number | 2008-021B |
| NORAD Number | 32784 |
| Comments | Technology development; carries innovative attitude sensor. |