On the Evection Resonance and Its Connection to the Stability of Outer Satellites

Figure 2

(a) Prograde satellite. Initial conditions: 𝑎=395𝑅_𝐽, 𝑒=0.01, 𝐼=1.5^∘, and 𝜛=180^∘. (b) Prograde satellite. Initial conditions: 𝑎=400𝑅_𝐽, 𝑒=0.1, 𝐼=1^∘ and 𝜛=180^∘.

(a)

(b)