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134389 (1996 VP2)
Classification: Main-belt Asteroid          SPK-ID: 2134389
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1632910842039143 5.3431e-08  
a 3.06905559118845 1.737e-08 au
q 2.567906176221203 1.687e-07 au
i .2526137492496545 5.5099e-06 deg
node 139.6684974417334 0.00096672 deg
peri 208.174057003876 0.0009668 deg
M 177.7948264787687 1.2855e-05 deg
tp 2458030.610677272712
(2017-Oct-04.11067727)		 6.6865e-05 TDB
period 1963.837548577482
5.38		 1.6672e-05
4.565e-08		 d
yr
n .1833145517870194 1.5562e-09 deg/d
Q 3.570205006155698 2.0206e-08 au
   Orbit Determination Parameters
   # obs. used (total)      844  
   data-arc span      10837 days (29.67 yr)  
   first obs. used      1990-08-16  
   last obs. used      2020-04-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52114  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 22:18:57  

Additional Information
 Earth MOID = 1.56128 au 
 Jupiter MOID = 1.85171 au 
 T_jup = 3.211 
[ 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 15.0   n/a MPO338172  
diameter diameter 7.560 km 0.630 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.037   0.011 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

134389 (1996 VP2)          Discovered 1996-Nov-10 by di Cicco, D. at Sudbury.
Reference: 20060907/Numbers.arcLast Updated: 2006-09-10

[ show close-approach data ]
Alternate Designations
 1996 VP2 = 1990 QO7 = 2000 KM84 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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