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The current orbit of Methone (S/2004 S 1)

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Abstract

The Cassini spacecraft discovered many close-in small satellites in Saturnian system, and several of them exhibit exotic orbital states due to interactions with Mimas and the oblateness of the planet. This work is devoted to Methone, which is currently involved in a 15:14 mean-motion resonance with Mimas. We give an in-deep study on the current orbit of Methone by analyzing and identifying the short, resonant and long-term gravitational perturbations on its orbit. In addition, we perform numerical integrations of full equations of motion of ensembles of close-in small bodies orbiting the non-central field of Saturn. Spectral analyses of the orbits and interpretation of them in dynamical maps allow us to describe the orbit and the dynamics of Methone in view of resonant and long-term dynamics. We show that the current geometric orbit of Methone is aligned with Mimas’ due to a forced resonant component in eccentricity, leading to simultaneous oscillations of several critical angles of the expanded disturbing function. Thus, we explain the simultaneous oscillations of four critical arguments associated to the resonance. The mapping of the Mimas–Methone resonance shows that the domains of the 15:14 Mimas–Methone resonance are dominated by regular motions associated to the Corotation resonance located at eccentricities lower than \(\sim \, 0.015\) and osculating semi-major axis in the interval 194,660–194,730 km. Methone is currently located deeply within this site.

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Notes

  1. We will define and denote the angles \(\psi _2\equiv 15\lambda _{\mathrm{Me}}-14\lambda _{\mathrm{M}}-\varpi _{\mathrm{Me}}\) and \(\psi _1\equiv 15\lambda _{\mathrm{Me}}-14\lambda _{\mathrm{M}}-\varpi _{M}\) by the Lindblad and corotation angles, respectively. This nomenclature comes from planetary ring dynamics (e.g., Murray and Dermott 1999).

  2. On the contrary to the example given above, the dynamics of the resonance 15:14 Mimas–Methone is dictated within the domain of the restricted three-body problem (El Moutamid et al. 2014), since the mass of Mimas is much larger than Methone’s.

  3. Recall that ephemerides are limited to a hundred of years, so that numerical simulations are able to cover the long-term components.

  4. This result has been shown in Callegari and Yokoyama (2020) in the case of the satellite Anthe, and the same should be directly applied to any other close-in small satellite of Saturn in Corotation resonance with Mimas.

  5. Recall that the forced eccentricity, roughly indicated by vertical dashed line, is measured from the center of the coordinate system, while the proper mode is taken from the forced center.

  6. The other initial elements in the simulation are the same than those of Methone at the date 2016-01-01; \(a_0=194{,}775\) km has been taken from Fig. 7. As discussed in item (i) in Sect. 5.1, at this initial conditions, the test particle is sufficiently far enough of the chaotic layers of the Corotation zone.

  7. Evidently, this conclusion is valid within in timescale utilized in this work (limited to tens of thousands of years).

  8. Exactly over the boundaries of the Corotation resonance, the continuations are broken, which is another possible indicator of chaoticity at the separatrices.

  9. For instance, by adopting \(P_{\Delta \varpi }=2408.21\) days and \(P_{\psi _1}=521.57\) days, we have \(P_{(\psi _1+\Delta \varpi )}=428.718\) days from the expression: \(\frac{1}{P_{(\psi _1+\Delta \varpi )}}=\frac{1}{P_{\psi _1}}+\frac{1}{P_{\Delta \varpi }}\).

  10. \(\chi \) is defined in equation 25 in El Moutamid et al. (2014), and its expression can be obtained from their Table 1. We utilize \(\chi =k\left[ \frac{ \sqrt{2} }{2} \left( \frac{a-a_0}{a_0}\right) +14e^2\left( \frac{ \sqrt{2} }{2}-1\right) \right] \), where ae are the osculating semi-major axis and orbital eccentricity of the test particle; k is a function of the masses, orbital elements of Mimas and \(\mathbf{a}_0\), the reference center of the Corotation zone, where we adopt \(\mathbf{a}_0=194{,}683\) km.

  11. There is another additional indirect test of our results: Fig. 9 was obtained from numerical simulations performed with the Mercury package (numerical scheme (ii) described in Sect. 2), whereas in the calculation of the dynamical map, we applied our own code (scheme (i)).

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Acknowledgements

We are grateful to Fapesp (Sao Paulo state research funding agency), through the processes 2019/15162-2, 2020/06807-7. We are especially grateful to two anonymous reviewers, who have made a detailed review of our work. We also thanks T. Yokoyama and M. T. dos Santos for discussions. T. Yokoyama is the main author of the program code utilized in this work to compute the geometric elements, which has been developed during the project of the work Callegari and Yokoyama (2020).

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Appendices

Appendix 1: Initial conditions and parameters

Table 3 gives the initial osculating elements and masses of the mid-sized satellites of Saturn and Methone provided by Horizons system of ephemerides at date January 01, 2016.

The physical data for Saturn are \(M_S=5.6834\times 10^{26}\) (kg) (mass), \(R_S=60,268\pm 4\) km (equatorial radius), \(J_2=0.01629071\) and \(J_4=-0.0009358\) (Jacobson et al. 2006b).

Table 3 Orbital elements and masses of Saturnian satellites taken from the Horizons system referred to date January 01, 2016, 00:00

Appendix 2: Critical arguments \(\psi _k\), \(5\le k\le 14\)

In this Appendix, we extend the interpretation of the critical arguments of the disturbing given in Sect. 3.1 in the case \(\psi _k\), \(k\ge 5\) (Fig. 10).

The plots of the critical arguments of the disturbing \(\psi _k\), \(k\ge 5\) are given in Fig. 10. All of these angles but \(\psi _7\), \(\psi _8\), \(\psi _{10}\), \(\psi _{11}\) do not have any physical relevance since their time variations are dominated by short-term perturbations in both osculating and geometric variables.

From Table 2, we have:

$$\begin{aligned} \psi _7= & {} \alpha -\varpi _{\mathrm{M}}-\varOmega _{\mathrm{Me}}+\varOmega _{\mathrm{M}}=\psi _1-\Delta \varOmega _{\mathrm{Me}-\mathrm{M}}, \end{aligned}$$
(11)
$$\begin{aligned} \psi _8= & {} \alpha -\varpi _{\mathrm{M}}+\varOmega _{\mathrm{Me}}-\varOmega _{\mathrm{M}}=\psi _1+\Delta \varOmega _{\mathrm{Me}-\mathrm{M}}, \end{aligned}$$
(12)

where \(\alpha =15\lambda _{\mathrm{Me}}-14\lambda _{\mathrm{M}}\). \(\psi _7\), \(\psi _8\) are driven by the coupling of the oscillation of the corotation angle \(\psi _1=\alpha -\varpi _{\mathrm{M}}\) with a slower long-term circulation of \(\Delta \varOmega _{\mathrm{Me}-\mathrm{M}}\). Both osculating and geometric \(\Delta \varOmega _{\mathrm{Me}-\mathrm{M}}\) circulate in prograde direction with a period of \(P_{\Delta \varOmega }\sim \, 2443.28\) days (recall from Sect. 3.2 that \(\Delta \varOmega _{\mathrm{Me}-\mathrm{M}}\) is not significantly affected by the induced short-term circulations due to \(J_2\)). The different signs of \(\Delta \varOmega _{\mathrm{Me}-\mathrm{M}}\) in (11), (12) cause the long-term circulation of \(\psi _7\), \(\psi _8\) to occur in the opposite directions.

From Table 2, we have:

$$\begin{aligned} \psi _{10}= & {} \psi _1-\Delta \varpi _{\mathrm{Me}-\mathrm{M}}-\Delta \varOmega _{\mathrm{Me}-\mathrm{M}}, \end{aligned}$$
(13)
$$\begin{aligned} \psi _{11}= & {} \psi _1-\Delta \varpi _{\mathrm{Me}-\mathrm{M}}+\Delta \varOmega _{\mathrm{Me}-\mathrm{M}}. \end{aligned}$$
(14)

Since the geometric \(\Delta \varpi _{\mathrm{Me}-\mathrm{M}}\) oscillates around zero, the evolutions of the geometric \(\psi _{10}\) and \(\psi _{7}\), and \(\psi _{11}\) and \(\psi _{8}\), are, respectively, very similar.

Fig. 10
figure 10

Figure 3, continued. \(\psi _k\), \(5\le k\le 14\) are defined in Table 2

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Callegari, N., Rodríguez, A. & Ceccatto, D.T. The current orbit of Methone (S/2004 S 1). Celest Mech Dyn Astr 133, 49 (2021). https://doi.org/10.1007/s10569-021-10045-5

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