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Several spacecrafts show an anomalous flyby. In a previous paper anon-prefered reference frame is studied moving uniformly relative to theprefered one. In this article the Doppler frequency residual is derived. Theprefered reference frame is given by the isotropy of the CMB and thenon-prefered one is the Earth. The resulting jump is much too small to explainthe measured anomalous flybys of the different spacecrafts. Therefore, thetransformations from the prefered frame to the non-prefered frame are replacedby the corresponding total differentials. A formula for the Doppler frequencyresidual is derived. It is applied to the prefered frame of the Earth and thenon-prefered frame of the rotating Earth. The resulting Doppler residualdepends on the direction of the velocity of the spacecraft and the position ofthe observer on the rotating Earth. It is similar to the experimental formulaof Anderson et al. which is independent of the position of the observer.

Anomalous Flyby in the Non-Prefered Reference Frame of the Rotating Earth