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JPL Small-Body Database Browser
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(2019 VB5)
Classification: Apollo [NEO]          SPK-ID: 3892775
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 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2092305956169403 4.8871e-05  
a 1.066533541596487 2.7726e-05 au
q .843382093442809 3.0204e-05 au
i .8754316469758903 0.00021219 deg
node 223.9535829617015 2.0797e-05 deg
peri 264.8449116370091 0.00053516 deg
M 125.0124299932267 0.0116 deg
tp 2458460.795337501037
(2018-Dec-08.29533750)
0.018411 TDB
period 402.3094223698533
1.10
0.015688
4.295e-05
d
yr
n .894833628005468 3.4894e-05 deg/d
Q 1.289684989750164 3.3528e-05 au
  Orbit Determination Parameters
   # obs. used (total)      26  
   data-arc span      4 days  
   first obs. used      2019-11-05  
   last obs. used      2019-11-09  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .59093  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-09 01:12:10  

Additional Information
 Earth MOID = .000751514 au 
 Jupiter MOID = 3.74475 au 
 T_jup = 5.764 
[ 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 31.675   .36515 1 autocmod 2.8

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