Nanosatellite has limited functi mass constraint from 1 to 10 kg. Therefore, t low cost, low mass, low dimension, and low p must be fulfilled in designing and choosing nanosatellite. To obtain wider coverage area the low dimension, camera array was used to p wider area. In this research, On Board Data implemented in FPGA used below 100% o resource. LUT-FF pairs was the most used res usage. OBDH also combined the image from e image with wider area. The FPGA and 4 cam milliwatt of power consumption, higher than system of SNAP-1 nanosatellite which used 1 consumption.

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