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JPL Small-Body Database Browser
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(2016 VE4)
Classification: Apollo [NEO]          SPK-ID: 3763552
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3731082605611946 0.0003547  
a 1.520444693261706 0.00083045 au
q .9531542184793319 1.9842e-05 au
i 5.401952220625536 0.0038811 deg
node 235.7624660240623 0.0013336 deg
peri 210.4181935673296 0.004288 deg
M 95.14982441990801 0.37124 deg
tp 2458419.507800405654
(2018-Oct-28.00780041)
0.55788 TDB
period 684.7852032434415
1.87
0.56103
0.001536
d
yr
n .5257122938621964 0.00043071 deg/d
Q 2.08773516804408 0.0011403 au
  Orbit Determination Parameters
   # obs. used (total)      39  
   data-arc span      2 days  
   first obs. used      2016-11-09  
   last obs. used      2016-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .46143  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:22:17  

Additional Information
 Earth MOID = .00102556 au 
 Jupiter MOID = 3.15441 au 
 T_jup = 4.421 
[ 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 26.4   n/a MPO389569  

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