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

Figure 11

Retrograde satellite. Initial conditions: 𝑎=528.4𝑅_𝐽, 𝑒=0.15, 𝐼=179^∘, 𝜔=90^∘, and Ω=180^∘.

(a)

(b)