| Name of Satellite, Alternate Names | Can-X5 |
| Country of Operator/Owner | Canada |
| Operator/Owner | University of Toronto Institute for Aerospace Studies |
| Users | Civil |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | Sun-Synchronous |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 643 |
| Apogee (km) | 656 |
| Eccentricity | 0.000925991879763516 |
| Inclination (degrees) | 98.26 |
| Period (minutes) | 97.72 |
| Launch Mass (kg.) | 15 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 30-06-2014 |
| Expected Lifetime | |
| Contractor | University of Toronto Institute for Aerospace Studies |
| Country of Contractor | Canada |
| Launch Site | Sriharikota Launch Station |
| Launch Vehicle | PSLV-CA |
| COSPAR Number | 2014-034D |
| NORAD Number | 40056 |
| Comments | Demonstrate formation flying by a pair of nanosatellites |