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(2020 FV3)
Classification: Apollo [NEO]          SPK-ID: 54016334
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 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1511558312655021 0.00021257  
a 1.025394586178074 9.1634e-05 au
q .8704002151291814 0.00014075 au
i 9.061258898069212 0.012364 deg
node 180.7752947604965 0.00041437 deg
peri 99.85258758265012 0.0085132 deg
M 344.1657375603364 0.023456 deg
tp 2459017.181315447763
(2020-Jun-16.68131545)
0.022476 TDB
period 379.2581804222097
1.04
0.050838
0.0001392
d
yr
n .9492214501457279 0.00012724 deg/d
Q 1.180388957226966 0.00010548 au
  Orbit Determination Parameters
   # obs. used (total)      23  
   data-arc span      3 days  
   first obs. used      2020-03-22  
   last obs. used      2020-03-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .69546  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-22 06:32:55  

Additional Information
 Earth MOID = .018064 au 
 Jupiter MOID = 3.89399 au 
 T_jup = 5.941 
[ 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 27.63   .41471 3 autocmod 2.8

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