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  APOSTLE transits of XO-2 system (Kundurthy+, 2013)
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1.J/ApJ/770/36/table10Data on the stability simulations of the XO-2 system (3600000 rows)

Query by Constraints constraints help applied on Columns (Output Order: + - )
ShowSortColumn  Constraint Explain   (UCD)
  SimID  (i) [0/3599999] Simulation identifier (Note 1)   (
  Mp Mgeo Mass of perturber; Earth masses (Note 2)   (phys.mass)
  a AU Semi-major axis (Note 2)   (phys.size.smajAxis)
  e  Eccentricity (Note 2)   (src.orbital.eccentricity)
  i deg Orbital inclination (Note 2)   (src.orbital.inclination)
  Omega deg Argument of pericenter (Note 2)   (src.orbital)
  omega deg Longitude of ascending node (Note 2)   (src.orbital.node)
  M deg Mean anomaly (Note 2)   (src.orbital.meanAnomaly)
  Stab   [0/1] Stability outcome (1=stable) (Note 3)   (meta.code)
  ECons   [0/2.7] Energy conservation (Note 3)   (
  stdTTV s (n) [0/370800] Standard deviation of transit timing variations (Note 3)   (stat.stdev)
  stdTDV  (n) [0/0.01] Standard deviation of transit depth variations (Note 3)   (stat.stdev)
  stdTBV  (n) [0/0.07] Standard deviation of transit impact parameter (b) variations (Note 3)   (stat.stdev)

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