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

Figure 16

Retrograde satellite. Initial conditions: 𝑎=612𝑅_𝐽, 𝑒=0.001, 𝐼=179^∘, 𝜔=180^∘, and Ω=0^∘.

(a)

(b)