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JPL Small-Body Database Browser
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(2018 VZ6)
Classification: Apollo [NEO]          SPK-ID: 3836177
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 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3238158477681709 0.00043257  
a 1.034507058932121 0.00024379 au
q .6995172786218589 0.0002828 au
i 9.230111798635221 0.014339 deg
node 221.8390389334432 0.00062424 deg
peri 290.5609524007579 0.0034234 deg
M 89.57249415640489 0.001284 deg
tp 2458504.875146881335
(2019-Jan-21.37514688)
0.032486 TDB
period 384.3249810886054
1.05
0.13585
0.0003719
d
yr
n .9367072600388751 0.00033111 deg/d
Q 1.369496839242383 0.00032273 au
  Orbit Determination Parameters
   # obs. used (total)      26  
   data-arc span      2 days  
   first obs. used      2018-11-09  
   last obs. used      2018-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .47048  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Nov-12 07:30:39  

Additional Information
 Earth MOID = .0227582 au 
 Jupiter MOID = 3.6479 au 
 T_jup = 5.863 
[ 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   .61102 E2018-VG6 autocmod 2.6q

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