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Table 2.

Mean values and standard deviations of a0 (in AU) and i0 (in degree) of the orbits selected for the numerical fitting for g and s, respectively in regions L, C, and R.

σa0 σi0
L 0.995040 0.00173011 9.29600 8.40849
g C 1.00002 0.00166711 17.0435 12.1155
R 1.00508 0.00176528 9.24342 8.35572

L 0.995299 0.00166176 13.8992 12.1669
s C 1.00002 0.00159960 26.5344 15.9284
R 1.00479 0.00169481 13.5209 12.0755

Notes. The quantities and stand for mean values while σa0 and σi0 stand for standard deviations. We adopt the double-precision floating-point format in our calculations but we only show 6 significant figures in this table for lack of space.

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