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JPL Small-Body Database Browser
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(2019 VS3)
Classification: Apollo [NEO]          SPK-ID: 3892701
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 .5431850766804917 0.0023441  
a 2.197311250821856 0.011422 au
q 1.003764570553279 6.7326e-05 au
i 1.096198414119479 0.0036014 deg
node 42.076611848647 0.00013519 deg
peri 354.817606313215 0.019901 deg
M 1.609543413121568 0.017719 deg
tp 2458788.180926514451
(2019-Oct-31.68092651)
0.018419 TDB
period 1189.695437343889
3.26
9.276
0.0254
d
yr
n .3025984539402244 0.0023593 deg/d
Q 3.390857931090432 0.017626 au
  Orbit Determination Parameters
   # obs. used (total)      17  
   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      .49823  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-06 15:42:18  

Additional Information
 Earth MOID = .0106748 au 
 Jupiter MOID = 2.04561 au 
 T_jup = 3.459 
[ 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 28.533   .3373 1 autocmod 2.8

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