Interesting couple.
Simulation based on nominal orbital parameters
Mercury6 software
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) Important integration parameters:
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algorithm (MVS, BS, BS2, RADAU, HYBRID etc) = BS
start time (days)= 2460106.5
) stop time (days) = 102458000.5
stop time (days) = -1e8
output interval (days) = 100
timestep (days) = 0.05
accuracy parameter=1.d-12
Simulation result
