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JPL Small-Body Database Browser
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(2019 VX)
Classification: Apollo [NEO]          SPK-ID: 3892279
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6077802334742791 6.9533e-05  
a 2.351175285486026 0.00040365 au
q .9221774215343744 5.167e-06 au
i 3.975307134624229 0.00029496 deg
node 238.9813391183642 0.0002879 deg
peri 207.05316111843 0.00017282 deg
M 47.35617901208722 0.012031 deg
tp 2458827.279179403688
(2019-Dec-09.77917940)
0.00060027 TDB
period 1316.818559173778
3.61
0.33911
0.0009284
d
yr
n .2733861833067401 7.0402e-05 deg/d
Q 3.780173149437678 0.00064898 au
  Orbit Determination Parameters
   # obs. used (total)      50  
   data-arc span      36 days  
   first obs. used      2019-10-07  
   last obs. used      2019-11-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .4125  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-03 19:59:42  

Additional Information
 Earth MOID = .00879941 au 
 Jupiter MOID = 1.48886 au 
 T_jup = 3.278 
[ 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 25.4   .28525 E2019-VE8 autocmod 2.8

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