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Fig. 1

Fig. 1 Refer to the following caption and surrounding text.

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Left panel: de-synchronizations (Δ*=τp*τsMathematical equation: ${\Delta ^*} = \tau _{\rm{p}}^* - {\tau _s}$) and frequency offsets (∆f) of four numerically simulated time-aligned orbits with different initial inclinations. Right panel: corrected Δc*=τp,c*τsMathematical equation: $\Delta _{\rm{c}}^* = \tau _{{\rm{p,c}}}^* - {\tau _s}$ and Δfc*Mathematical equation: $\Delta f_{\rm{c}}^*$ for the same four simulated orbits by accounting for the deviation of the mean orbital elements in our simulations from the ones required by the time-aligned orbits.

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