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Table 2

Leading amplitudes and periods characterizing the orbital elements e,M, and Ls.

Orbital element Period Amplitude Amplitude
sin cos
days

501.078 7.1200 × 10-4 5.776 × 10-3
eccentricity 3505.99 1.4949 × 10-3 8.19196 × 10-4
e 550.62 1.260 × 10-3 –8.9235 × 10-4

498.88 2.4850 –0.488
mean anomaly 553.38 0.5212 0.2515
M 177.50 1.20 × 10-2 –0.2338

262.02 –0.2959 –0.2669
mean longitude 499.25 0.3470 –5.2116 × 10-2
LS 554.2945 6.7272 × 10-2 7.1011 × 10-4

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