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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3238613778414271 0.00043256  
a 1.034590046429867 0.00024309 au
q .6995262884920639 0.0002833 au
i 9.229835092688587 0.014341 deg
node 221.8282015274544 0.00066842 deg
peri 290.5430022829772 0.0033131 deg
M 104.2811253400709 0.13366 deg
tp 2458889.159266251839
(2020-Feb-09.65926625)
0.10347 TDB
period 384.371227474046
1.05
0.13547
0.0003709
d
yr
n .9365945582498325 0.00033009 deg/d
Q 1.369653804367669 0.00032182 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 = .0229328 au 
 Jupiter MOID = 3.64627 au 
 T_jup = 5.862 
[ 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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