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) |