Fig. 5

image

Apparent motion of 50 satellite clones in the correlated frame from the first image of run 1 to the last image of run 5. The arrow orientation indicates the direction of the apparent motion in the CCD frame taking into account the spacecraft position and pointing as included in the spice kernels and a random velocity lower than the escape velocity. The arrow length provides an indication of the total displacement on the CCD frame due to the satellite clone motion.

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