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(2019 VH5)
Classification: Apollo [NEO]          SPK-ID: 3892802
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 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .363990494651616 0.00014877  
a 1.105948192765708 0.00010731 au
q .703393563021857 9.6287e-05 au
i 4.680184365083611 0.0021705 deg
node 65.51984072716125 0.00074765 deg
peri 102.5907538967425 0.0023265 deg
M 94.60249167490042 0.0072198 deg
tp 2458888.864923023429
(2020-Feb-09.36492302)
0.0077277 TDB
period 424.8157421653652
1.16
0.061828
0.0001693
d
yr
n .8474262233433553 0.00012333 deg/d
Q 1.508502822509558 0.00014636 au
  Orbit Determination Parameters
   # obs. used (total)      90  
   data-arc span      26 days  
   first obs. used      2019-11-08  
   last obs. used      2019-12-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .42115  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jan-04 05:11:44  

Additional Information
 Earth MOID = .0116691 au 
 Jupiter MOID = 3.46502 au 
 T_jup = 5.561 
[ 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 23.2   .44349 E2020A55 autocmod 2.8

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