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(2010 WG3)
Classification: Apollo [NEO]          SPK-ID: 3552575
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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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 .1462603466146941 1.5245e-06  
a 1.00874496927304 6.346e-08 au
q .8612055804213363 1.4932e-06 au
i 13.50274292561921 0.00010325 deg
node 71.55451292861792 2.0739e-05 deg
peri 217.7334486659249 0.00020482 deg
M 263.4516152955485 0.00040256 deg
tp 2459099.745999795642
(2020-Sep-07.24599980)
0.00042089 TDB
period 370.0585984509361
1.01
3.492e-05
9.561e-08
d
yr
n .9728189035654315 9.18e-08 deg/d
Q 1.156284358124744 7.2741e-08 au
  Orbit Determination Parameters
   # obs. used (total)      73  
   data-arc span      362 days  
   first obs. used      2010-11-27  
   last obs. used      2011-11-24  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      2  
   norm. resid. RMS      .36489  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:55:35  

Additional Information
 Earth MOID = .113983 au 
 Jupiter MOID = 3.93007 au 
 T_jup = 6.005 
[ show covariance matrix ]

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 22.8   n/a MPO213453  

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