You signed in with another tab or window. Reload to refresh your session.You signed out in another tab or window. Reload to refresh your session.You switched accounts on another tab or window. Reload to refresh your session.Dismiss alert
The integrated orbits use x0 and v0 (initial position/velocity), instead of e and a (eccentricity/semi-major axis), so the probability/model generation functions need to be updated to account for this
The text was updated successfully, but these errors were encountered:
The integrated orbits use x0 and v0 (initial position/velocity), instead of e and a (eccentricity/semi-major axis), so the probability/model generation functions need to be updated to account for this
The text was updated successfully, but these errors were encountered: