| FOV | 2.86° |
| IFOV (nadir) | 17.16 μrad |
| Pixel scale at 100-km altitude | 1.7 meter |
| Max. swath size at 100-km altitude | 5.2 km × 144 km |
| f/# | 3.6 |
| Focal length | 699.275 ± 0.01 mm |
| Distortion coefficient k | 0.0000174 ± 0.00000057 |
| Optical center location sample | 1558 (1545, 1572 95% bounds) |
| Primary mirror diameter | 195 mm |
| Aperture | 194.4 mm |
| System MTF (Nyquist) | 0.21 |
| Gain | 23 to 30 e−/DN |
| Read noise | 60 e− |
| Detector full-well (shallow, deep) | 94,000; 123,000 e− |
| S/N (@ 0.12 W/m2/sr/um) | 100 |
| Spectral response | 410–780 nm |
| Radiometric accuracy | 1% relative, 6% absolute |
| Active pixels | 3,072 |
| Maximum lines | 84,992 |
| Detector digitization | 12 bit, encoded to 8 bit |
| Data link to spacecraft | 4 Mbps |
| Temperature sensors | 4 |
| Voltage | 28 ± 7 V DC |
| Peak power | 9.3 W |
| Standby power | 4.5 W |
| Mass | 8.75 kg |
| Volume (length × diameter) | 118 cm × 27 cm (incl. radiator) |