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JPL Small-Body Database Browser
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(2019 VM2)
Classification: Apollo [NEO]          SPK-ID: 3892659
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 2458791.5 (2019-Nov-04.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2390573584512837 0.0006654  
a 1.267860630609477 0.0011155 au
q .9647692173715964 4.2606e-05 au
i 26.28899294305405 0.034651 deg
node 220.8818125754452 0.00016235 deg
peri 144.0949927359635 0.042103 deg
M 21.97129077467312 0.058609 deg
tp 2458759.675706401560
(2019-Oct-03.17570640)
0.044127 TDB
period 521.4416309416326
1.43
0.68817
0.001884
d
yr
n .690393667551827 0.00091114 deg/d
Q 1.570952043847357 0.0013822 au
  Orbit Determination Parameters
   # obs. used (total)      18  
   data-arc span      1 day  
   first obs. used      2019-11-04  
   last obs. used      2019-11-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .43713  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-05 09:12:03  

Additional Information
 Earth MOID = .009132 au 
 Jupiter MOID = 3.93095 au 
 T_jup = 4.964 
[ 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 27.004   .50391 1 autocmod 2.8

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