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

Figure 5

(a) Retrograde satellite. Initial conditions: 𝑎=520𝑅_𝐽, 𝑒=0.03, 𝐼=176^∘, 𝜔=0^∘, and Ω=90^∘. (b) Retrograde satellite. Initial conditions: 𝑎=520𝑅_𝐽, 𝑒=0.03, 𝐼=176^∘, 𝜔=90^∘, and Ω=0^∘.

(a)

(b)