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(2019 VD3)
Classification: Apollo [NEO]          SPK-ID: 3892689
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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6042395675810825 0.00017381  
a 2.450600557965811 0.0010615 au
q .9698507365065895 5.8537e-06 au
i 1.680457007597352 0.00035051 deg
node 227.4699283882171 0.00020917 deg
peri 152.9761661115451 0.0011948 deg
M 57.68775678377085 0.037554 deg
tp 2458775.962765320949
(2019-Oct-19.46276532)
0.00031375 TDB
period 1401.222876241205
3.84
0.91047
0.002493
d
yr
n .2569184432427365 0.00016694 deg/d
Q 3.931350379425032 0.001703 au
  Orbit Determination Parameters
   # obs. used (total)      167  
   data-arc span      3 days  
   first obs. used      2019-11-05  
   last obs. used      2019-11-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .38687  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-14 09:20:32  

Additional Information
 Earth MOID = .00369448 au 
 Jupiter MOID = 1.53783 au 
 T_jup = 3.216 
[ 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 25.9   .46098 E2019-VI7 autocmod 2.8

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