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Table 4

Orbital parameters estimated from the three trajectories of the second follow-up campaign corresponding to Jupiter satellites, considering Jupiter as the center of mass.

a [AU] e i [deg] U
1 0.233 ± 2.70 0.941 ± 0.235 97.7 ± 2.9 10.2
2 0.103 ± 1.98 0.341 ± 0.198 153.2 ± 0.28 10.2
3 0.168 ± 0.448 0.225 ± 4.18 159 ± 23 13.1

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