Deimos-2 was developed and integrated by Elecnor Deimos Satellite Systems (Spain), in cooperation with SATREC Initiative (South Korea).
Deimos-2 satellite was launched on June 19, 2014 on a Dnepr vehicle from the Yasny Cosmodrome (Russia). It operates from a sun-synchronous orbit at an altitude of 620 km and provides panchromatic images with 1 m resolution and multispectral images with 4 m resolution.
The average revisit time of Deimos-2 is 4 days and it can capture up to 200,000 km² per day. Swath width is 12 km. Recording equipment: HiRAIS / EOS-D. The satellite is able to swivel 30 degrees off nadir to each side, and 45 degrees in the event of a special order.
Technical Characteristics
| Modes: | Panchromatic | Multispectral |
| Spectral Range (µm): | 0,56–0,90 | blue: 0.46–0.52 green: 0.53-0.60 red: 0.64-0.70 near infrared: 0.77-0.89 |
| Spatial Resolution, m: | 1 | 4 |
| Radiometric Resolution: | 10 bits / pixel | |
| Swath Width: | 12 km | |
| Revisit time: | 2 days (at +/-45 °) | |
| Geometric accuracy: | CE 90 100 m w/o GCP | |
| Acquire Stereo-Pair: | Yes, from one pass | |