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32427 (2000 RU68)
Classification: Main-belt Asteroid          SPK-ID: 2032427
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1825297249221243 3.8418e-08  
a 3.073338358902301 1.9228e-08 au
q 2.512362753659251 1.1209e-07 au
i 3.676251166410072 4.0254e-06 deg
node 111.1190385007217 8.1002e-05 deg
peri 1.002338432300464 8.2285e-05 deg
M 72.63572162469139 1.537e-05 deg
tp 2458203.434872645116
(2018-Mar-25.93487264)
8.2432e-05 TDB
period 1967.949689910793
5.39
1.8469e-05
5.057e-08
d
yr
n .1829315057420593 1.7168e-09 deg/d
Q 3.634313964145351 2.2738e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1203  
   data-arc span      9875 days (27.04 yr)  
   first obs. used      1992-04-27  
   last obs. used      2019-05-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54104  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 03:43:45  

Additional Information
 Earth MOID = 1.52921 au 
 Jupiter MOID = 1.48683 au 
 T_jup = 3.201 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 13.9   n/a MPO302254  
diameter diameter 6.995 km 0.533 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.131   0.030 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

32427 (2000 RU68)          Discovered 2000-Sep-02 by LINEAR at Socorro
Reference: 20011130/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 RU68 = 1992 HC7 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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