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(2020 FB5)
Classification: Apollo [NEO]          SPK-ID: 54016366
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 2458933.5 (2020-Mar-25.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .8430846728799628 0.00068777  
a 1.602217066032988 0.0044159 au
q .2514124150338725 0.00040904 au
i 3.096010331528752 0.0045862 deg
node 170.1751817844916 0.0038809 deg
peri 243.5832589646832 0.015466 deg
M 21.27707446229686 0.10623 deg
tp 2458889.718577354855
(2020-Feb-10.21857735)
0.037579 TDB
period 740.7650041447835
2.03
3.0624
0.008384
d
yr
n .485984081302034 0.0020091 deg/d
Q 2.953021717032103 0.0081388 au
  Orbit Determination Parameters
   # obs. used (total)      121  
   data-arc span      9 days  
   first obs. used      2020-03-24  
   last obs. used      2020-04-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .41828  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-03 06:34:51  

Additional Information
 Earth MOID = .0120812 au 
 Jupiter MOID = 2.44184 au 
 T_jup = 3.844 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 4.730217646010302E-7 -2.813215674772089E-7 2.584578021995582E-5 2.516955298291374E-6 -1.061127494958715E-5 3.14974956467291E-6
q -2.813215674772089E-7 1.673159434209057E-7 -1.537132187339872E-5 -1.495037269080932E-6 6.309786312309118E-6 -1.872922627033874E-6
tp 2.584578021995582E-5 -1.537132187339872E-5 .001412206685506383 .0001375400628698841 -.0005798093454939607 .0001721039504983872
node 2.516955298291374E-6 -1.495037269080932E-6 .0001375400628698841 1.506124058263456E-5 -5.781300241679683E-5 1.707428643523169E-5
peri -1.061127494958715E-5 6.309786312309118E-6 -.0005798093454939607 -5.781300241679683E-5 .0002392055884476705 -7.091557818394322E-5
i 3.14974956467291E-6 -1.872922627033874E-6 .0001721039504983872 1.707428643523169E-5 -7.091557818394322E-5 2.103319560333566E-5

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 24.76   .33628 4 autocmod 2.8

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Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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