| Auto: | all |
| NEE-02 Krysaor | |
| Mission Type: | Technology demonstration |
| Cospar Id: | 2013-066AB |
| Satcat: | 39441 |
| Mission Duration: | Design: 1 year Elapsed: |
| Orbits Completed: | 15,074[1] |
| Spacecraft Type: | 1U CubeSat |
| Manufacturer: | Ecuadorian Civilian Space Agency |
| Launch Mass: | 1.2kg (02.6lb) |
| Dimensions: | 10* |
| Power: | 127 watts maximum |
| Launch Date: | UTC |
| Launch Rocket: | Dnepr |
| Launch Site: | Dombarovsky 370/13 |
| Entered Service: | 25 January 2014 |
| Orbit Epoch: | 10 September 2016, 08:01:29 UTC |
| Orbit Reference: | Geocentric |
| Orbit Regime: | Sun-synchronous |
| Orbit Periapsis: | 588.13km (365.45miles) |
| Orbit Apoapsis: | 705.58km (438.43miles) |
| Orbit Inclination: | 97.6637 degrees |
| Orbit Semimajor: | 7024.99km (4,365.13miles) |
| Orbit Eccentricity: | 0.0083597 |
| Orbit Period: | 97.66 minutes |
| Orbit Mean Motion: | 14.74 |
| Apsis: | gee |
NEE-02 Krysaor is an Ecuadorian technology demonstration satellite, and Ecuador's second satellite launched to space. Built by the Ecuadorian Civilian Space Agency (EXA), it is a single-unit CubeSat nanosatellite. Krysaor is a Pegasus-class spacecraft, a "twin" of Ecuador's first satellite, NEE-01 Pegaso. Like Pegaso, this spacecraft's instruments include a dual visible and infrared camera which allows the spacecraft to take pictures and transmit live video from space.