VizieR

CfA VizieR . ADAC VizieR . Cambridge (UK) VizieR . IUCAA VizieR . INASAN VizieR .

VizieR

  
J/AJ/163/91
  Parameters & dynamic solutions of Kepler planets (Judkovsky+, 2022)
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1.J/AJ/163/91/tablea1Physical and orbital elements of our solutions that pass all tests (261 rows)

Simple ConstraintList Of Constraints
 
Query by Constraints constraints help applied on Columns (Output Order: + - )
ShowSortColumn  Constraint Explain   (UCD)
  recno  Record number assigned by the VizieR team. Should Not be used for identification. (meta.record)
  Adopted   [0/1] Adopted solution (1=yes) (meta.code)
  ID   [1/5] Solution identifier (meta.id)
  Kepler (char) (i) Kepler star identifier (meta.id;meta.main)
  m_Kepler (char) Kepler identifier component for the planet (meta.code.multip)
  KOI   [41.01/2711.02] Kepler Object of Interest identifier (meta.id)
  Per d [1.73/160.02] Mean orbital period (time.period;stat.mean)
  Mp/Ms ppm [1.63/1429] Planet-to-star mass ratio (phys.mass;arith.ratio)
  E_Mp/Ms ppm [0.21/58] Upper uncertainty on Mp/Ms (stat.error;stat.max;phys.mass)
  e_Mp/Ms ppm [-67/-0.25] Lower uncertainty on Mp/Ms (stat.error;stat.min;phys.mass)
  Mp geoMass [0.39/597] Absolute planet mass; derived from Mp/Ms and literature stellar mass (phys.mass)

ALL cols		    
 (i)indexed column
  E_Mp geoMass [0.17/37] Upper uncertainty on Mp (stat.error;stat.max;phys.mass)
  e_Mp geoMass [-45/-0.14] Lower uncertainty on Mp (stat.error;stat.min;phys.mass)
  rhop g/cm3 [0.08/49] Absolute planet density; derived from RhoRel and literature stellar density (phys.density)
  E_rhop g/cm3 [0.015/20] Upper uncertainty on rhop (stat.error;stat.max;phys.density)
  e_rhop g/cm3 [-45/-0.014] Lower uncertainty on rhop (stat.error;stat.min;phys.density)
  Rp Rgeo [0.96/12.05] Absolute planet radius; derived from ror and literature stellar radius (phys.size.radius)
  E_Rp Rgeo [0.019/0.55] Upper uncertainty on Rp (stat.error;stat.max;phys.size.radius)
  e_Rp Rgeo [-0.48/-0.021] Lower uncertainty on Rp (stat.error;stat.min;phys.size.radius)
  dex   [-0.18/0.24] Eccentricity difference to preceding planet; x is pointing at the observer (src.orbital.eccentricity)
  E_dex   [2e-3/0.13] Upper uncertainty on dex (stat.error;stat.max;src.orbital.eccentricity)
  e_dex   [-0.2/2.1e-3] Lower uncertainty on dex (stat.error;stat.min;src.orbital.eccentricity)
  dey   [-0.25/0.41] Eccentricity difference to preceding planet; y is the direction perpendicular to the line of sight pointing with the planets motion along transit (src.orbital.eccentricity)
  E_dey   [1.8e-3/0.15] Upper uncertainty on dey (stat.error;stat.max;src.orbital.eccentricity)
  e_dey   [-0.43/-2e-3] Lower uncertainty on dey (stat.error;stat.min;src.orbital.eccentricity)
  ix deg [-29/35] ix=i*cos(Omega) is the inclination component corresponding to the inclination around to the line of sight ("roll angle") (src.orbital.inclination)
  E_ix deg [0/22.6] Upper uncertainty on ix (stat.error;stat.max;src.orbital.inclination)
  e_ix deg [-20.1/0] Lower uncertainty on ix (stat.error;stat.min;src.orbital.inclination)
  iy deg [-4.4/7.1] iy=i*sin(Omega) is the inclination component corresponding to the inclination relative to the line of sight (src.orbital.inclination)
  E_iy deg [5.8e-3/6.14] Upper uncertainty on iy (stat.error;stat.max;src.orbital.inclination)
  e_iy deg [-2.33/-5e-3] Lower uncertainty on iy (stat.error;stat.min;src.orbital.inclination)

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