| Name of Satellite, Alternate Names | UKube-1 (UK Cubesat 1) |
| Country of Operator/Owner | United Kingdom |
| Operator/Owner | UK Space Agency |
| Users | Government |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 626 |
| Apogee (km) | 631 |
| Eccentricity | 0.000357219404158034 |
| Inclination (degrees) | 98.4 |
| Period (minutes) | 97.27 |
| Launch Mass (kg.) | 3 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 08-07-2014 |
| Expected Lifetime | |
| Contractor | Clyde Space |
| Country of Contractor | United Kingdom |
| Launch Site | Baikonur Cosmodrome |
| Launch Vehicle | Soyuz-2.1b |
| COSPAR Number | 2014-037F |
| NORAD Number | 40074 |
| Comments | Technology demonstrator to show how impacts from cosmic particles can be used to increase the security of satellite communications. |