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  La2010: orbital solution for long term Earth motion (Laskar+ 2011)
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1.J/A+A/532/A89/orbitKeplerian elements of the Earth orbit for the solutions La2010a, La2010b, La2010c, and La2010a every 1kyr [model](plot of the orbital variations) (1000000 rows)

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ShowSortColumn  Constraint Explain   (UCD)
  S (char) Solution (a, b, c or d): their differences reflect the uncertainty in the solution [not valid beyond 50Myr] (;
  t Myr (i) [-249999/0] Time from J2000.0 (time.epoch)
  a AU Semi-major axis (Note 1)   (phys.angSize.smajAxis;src.orbital)
  l rad Mean longitude (expressed in radians) (Note 1)   (src.orbital.periastron)
  k  e*cos(ϖ) (Note 1)   (src.orbital)
  h  e*sin(ϖ) (Note 1)   (src.orbital)
  q  sin(i/2)cos(Ω) (Note 1)   (src.orbital)
  p  sin(i/2)sin(Ω) (Note 1)   (src.orbital)
  i deg Inclination angle i = sin–1(sqrt(p2+q2)) (Note 1)   (src.orbital.inclination)
  e  Eccentricity [sqrt(k2+h2)] (src.orbital.eccentricity)

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