| Name of Satellite, Alternate Names | Dove-2 |
| Country of Operator/Owner | USA |
| Operator/Owner | Planet Labs, Inc. |
| Users | Commercial |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | Sun-Synchronous |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 559 |
| Apogee (km) | 582 |
| Eccentricity | 0.00165694114256898 |
| Inclination (degrees) | 64.88 |
| Period (minutes) | 96.08 |
| Launch Mass (kg.) | 5.8 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 19-04-2013 |
| Expected Lifetime | .5 yrs. |
| Contractor | Planet Labs, Inc. |
| Country of Contractor | USA |
| Launch Site | Baikonur Cosmodrome |
| Launch Vehicle | Soyuz 2-1A |
| COSPAR Number | 2013-015C |
| NORAD Number | 39132 |
| Comments | Remote sensing; also an internal company technology demonstration experiment to test the capabilities of a low-cost spacecraft constrained to the 3U cubesat form factor to host a small payload. |