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183338 (2002 VM83)
Classification: Main-belt Asteroid          SPK-ID: 2183338
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 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1663836478093832 5.1663e-08  
a 2.567932097289258 1.8263e-08 au
q 2.140670187615472 1.3197e-07 au
i 15.01588151442886 4.7057e-06 deg
node 75.32993047341299 2.865e-05 deg
peri 345.0374041604425 3.824e-05 deg
M 95.02491175515243 2.8218e-05 deg
tp 2458603.757519202617
(2019-Apr-30.25751920)
0.00011515 TDB
period 1503.051046814717
4.12
1.6034e-05
4.39e-08
d
yr
n .239512823441969 2.5551e-09 deg/d
Q 2.995194006963045 2.1302e-08 au
  Orbit Determination Parameters
   # obs. used (total)      375  
   data-arc span      6390 days (17.49 yr)  
   first obs. used      2002-10-31  
   last obs. used      2020-04-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .60803  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-21 04:37:57  

Additional Information
 Earth MOID = 1.1572 au 
 Jupiter MOID = 2.33474 au 
 T_jup = 3.364 
[ 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 16.1   n/a MPO417990  
diameter diameter 2.078 km 0.492 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.148   0.026 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

183338 (2002 VM83)          Discovered 2002-Nov-07 by LINEAR at Socorro
Reference: 20080420/Numbers.arcLast Updated: 2008-04-23

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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