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Table 2

Comparison of nominal mean orbital elements (σ¯pMathematical equation: ${{\bar \sigma }_{\rm{p}}}$) and mean orbital elements (σ¯p*Mathematical equation: $\bar \sigma _{\rm{p}}^*$) from our numerical simulations with σ = {a, e, i}.

Number āp [km] ēp īp a¯pMathematical equation: $\bar a_{\rm{p}}^ * $ [km] e¯pMathematical equation: $\bar e_{\rm{p}}^ * $ i¯pMathematical equation: $\bar i_{\rm{p}}^ * $ [ns] f Δc*Mathematical equation: $\Delta _{\rm{c}}^*$ [ns] Δfc*Mathematical equation: $\Delta f_{\rm{c}}^*$
1 2606.2658 0 0 2606.1094 0.0039 1.907 50 1.6 × 10−15 −6 −2 × 10−16
2 2606.1186 0 25 2605.9063 0.0056 23.395 70 2.3 × 10−15 −13 −4 × 10−16
3 2605.7163 0 54.736 2605.3468 0.0046 53.475 140 4.4 × 10−15 −9 −3 × 10−16
4 2605.4477 0 85 2604.9803 0.0040 84.715 190 6.0 × 10−15 9 3 × 10−16

Notes. In our simulations, we adopted each initial state as σp,0=σ¯pMathematical equation: ${\sigma _{{\rm{p}},0}} = {{\bar \sigma }_{\rm{p}}}$. The resulting and corrected frequency offsets and de-synchronizations are also listed. The de-synchronizations ∆ and Δc*Mathematical equation: $\Delta _{\rm{c}}^*$ are shown as their values at the end of a year.

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