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32492 (2000 VJ15)
Classification: Main-belt Asteroid          SPK-ID: 2032492
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 31 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2193818378176528 3.8042e-08  
a 2.791749054200238 1.4852e-08 au
q 2.179290015964096 1.048e-07 au
i 10.57022261048095 4.5486e-06 deg
node 64.83244900420061 2.1896e-05 deg
peri 199.6426205907536 2.4397e-05 deg
M 203.2971030690889 1.2044e-05 deg
tp 2459742.130390266900
(2022-Jun-11.63039027)
5.8231e-05 TDB
period 1703.777950026005
4.66
1.3596e-05
3.722e-08
d
yr
n .2112951397184741 1.6862e-09 deg/d
Q 3.40420809243638 1.8111e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2662  
   data-arc span      8096 days (22.17 yr)  
   first obs. used      1998-02-24  
   last obs. used      2020-04-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .38661  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 07:27:28  

Additional Information
 Earth MOID = 1.16695 au 
 Jupiter MOID = 1.69031 au 
 T_jup = 3.269 
[ 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 13.2   n/a MPO365637  
diameter diameter 5.372 km 0.292 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.423   0.062 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

32492 (2000 VJ15)          Discovered 2000-Nov-01 by LINEAR at Socorro
Reference: 20011130/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 VJ15 = 1998 FE89 = 1999 SX6 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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