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(2020 FK3)
Classification: Apollo [NEO]          SPK-ID: 54016318
[ 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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5050525248997816 0.00059767  
a 1.920808822595005 0.0022249 au
q .9506994768936212 4.6791e-05 au
i 2.596626518539382 0.0026492 deg
node 164.7269305156466 0.00096509 deg
peri 64.52346945797885 0.0026629 deg
M 85.01882635187616 0.14627 deg
tp 2458970.865442999950
(2020-May-01.36544300)		 0.0039266 TDB
period 972.3545250774165
2.66		 1.6895
0.004626		 d
yr
n .3702353315744971 0.00064328 deg/d
Q 2.890918168296389 0.0033486 au
   Orbit Determination Parameters
   # obs. used (total)      83  
   data-arc span      15 days  
   first obs. used      2020-03-22  
   last obs. used      2020-04-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .43647  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-06 05:50:25  

Additional Information
 Earth MOID = .0239797 au 
 Jupiter MOID = 2.10538 au 
 T_jup = 3.757 
[ 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 25.3   .69024 E2020G66 autocmod 2.8

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