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JPL Small-Body Database Browser
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(2016 VX1)
Classification: Apollo [NEO]          SPK-ID: 3763337
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 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5387451330997215 1.6534e-05  
a 1.200459317165103 1.7824e-05 au
q .5537177025581889 1.1643e-05 au
i 3.503880993938703 0.00015984 deg
node 54.41674426614179 0.00015764 deg
peri 102.7790614225893 0.00057942 deg
M 268.4147758824817 0.013443 deg
tp 2458722.720064510834
(2019-Aug-27.22006451)
0.020662 TDB
period 480.4183605801102
1.32
0.010699
2.929e-05
d
yr
n .7493468808421399 1.6689e-05 deg/d
Q 1.847200931772017 2.7426e-05 au
  Orbit Determination Parameters
   # obs. used (total)      21  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      9 days  
   first obs. used      2016-11-04  
   last obs. used      2016-11-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .47301  
   source      ORB  
   producer      OSOD/JPL  
   solution date      2017-Jul-07 16:04:01  

Additional Information
 Earth MOID = .00218825 au 
 Jupiter MOID = 3.14818 au 
 T_jup = 5.142 
[ 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 25.0   n/a MPO389563  

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