Fig. 6.
Orbital evolution of the fictitious Earth Trojan indicated in Fig. 5 with the initial condition of a0 = 0.9999 AU, i0 = 27°. From top to bottom panels: evolutions of the apsidal differences between the Trojan and Mars Δϖ4, the argument of the perihelion ω and eccentricity e. The red vertical dashed lines in the bottom panel indicate the lifespan of the orbit.
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