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JPL Small-Body Database Browser
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(2019 VP3)
Classification: Apollo [NEO]          SPK-ID: 3892698
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 2458793.5 (2019-Nov-06.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2745551897769729 0.00096028  
a 1.173287027295793 0.001145 au
q .8511549848537361 0.00029605 au
i 11.93041509398483 0.038879 deg
node 223.4307212633246 0.00098168 deg
peri 255.3923049367723 0.023716 deg
M 312.6364044401821 0.11191 deg
tp 2458854.572682130815
(2020-Jan-06.07268213)
0.054905 TDB
period 464.1996729181159
1.27
0.67954
0.00186
d
yr
n .7755283361940313 0.0011353 deg/d
Q 1.49541906973785 0.0014594 au
  Orbit Determination Parameters
   # obs. used (total)      15  
   data-arc span      1 day  
   first obs. used      2019-11-05  
   last obs. used      2019-11-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .57014  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-06 15:42:08  

Additional Information
 Earth MOID = .0153937 au 
 Jupiter MOID = 3.6315 au 
 T_jup = 5.328 
[ 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 28.085   .22978 1 autocmod 2.8

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