Table 2
Comparison of nominal mean orbital elements (
) and mean orbital elements (
) from our numerical simulations with σ = {a, e, i}.
| Number | āp [km] | ēp | īp | [km] |
![]() |
![]() |
∆∗ [ns] | ∆f∗ | [ns] |
![]() |
|---|---|---|---|---|---|---|---|---|---|---|
| 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
. The resulting and corrected frequency offsets and de-synchronizations are also listed. The de-synchronizations ∆∗ and
are shown as their values at the end of a year.
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