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Table 14

Relative errors of calculated heliocentric orbital elements, given as a percent.

Group a(JPL) a(ESA) e(JPL) e(ESA) i(JPL) i(ESA) ω(JPL) ω(ESA) Ω(JPL) Ω(ESA)
Comet 7.715 7.449 4.812 4.169 2.807 2.711 0.569 0.563 0.005 0.007
Ryugu/Bennu 11.143 10.887 6.783 6.153 4.360 4.266 0.543 0.537 0.005 0.007
C-type 13.907 13.659 8.493 7.875 5.724 5.631 0.519 0.513 0.005 0.006
S-type 16.016 15.774 9.884 9.275 6.837 6.745 0.499 0.493 0.005 0.006
M-type 17.762 17.525 11.073 10.472 7.813 7.723 0.481 0.475 0.005 0.006
No-air 20.678 20.449 13.203 12.617 9.562 9.473 0.447 0.441 0.004 0.006

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