Research Article

A Comparison of Averaged and Full Models to Study the Third-Body Perturbation

Figure 14

Behavior of the orbital elements for an initial inclination of 130 degrees. The values for the eccentricity are 0.01, 0.05, 0.10, 0.50, 0.70, and 0.90. The initial conditions are a = 0.341 canonical units, M 0(0) = 0, ω(0) = 0, and Ω(0) = 0.
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