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(2019 VE2)
Classification: Apollo [NEO]          SPK-ID: 3892654
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 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2979884704603838 0.00045412  
a 1.422133641393977 0.00094427 au
q .9983542128047301 1.871e-05 au
i 5.158563675372319 0.0066095 deg
node 225.7471750042487 0.0010128 deg
peri 196.8008471994209 0.0067637 deg
M 110.1935819007838 0.10637 deg
tp 2458810.889300056318
(2019-Nov-23.38930006)
0.0070423 TDB
period 619.4539718400799
1.70
0.61696
0.001689
d
yr
n .5811569807690872 0.00057881 deg/d
Q 1.845913069983224 0.0012256 au
  Orbit Determination Parameters
   # obs. used (total)      15  
   data-arc span      2 days  
   first obs. used      2019-11-03  
   last obs. used      2019-11-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .55493  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-05 08:12:04  

Additional Information
 Earth MOID = .0160461 au 
 Jupiter MOID = 3.47814 au 
 T_jup = 4.653 
[ 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 27.4   .33386 MPO502151 autocmod 2.8

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