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(2020 TE6)
Classification: Apollo [NEO]          SPK-ID: 54065913
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 .5397221510142035 0.00045365  
a 1.941455174215039 0.0017849 au
q .8936088114900431 5.9173e-05 au
i 1.849154802965861 0.0012168 deg
node 24.91409621288949 0.00013384 deg
peri 45.53400706344207 0.00079629 deg
M 296.5205902889252 0.089805 deg
tp 2459174.728764627149
(2020-Nov-21.22876463)
0.0062125 TDB
period 988.0740156730028
2.71
1.3626
0.003731
d
yr
n .3643451748448163 0.00050246 deg/d
Q 2.989301536940036 0.0027483 au
  Orbit Determination Parameters
   # obs. used (total)      35  
   data-arc span      2 days  
   first obs. used      2020-10-15  
   last obs. used      2020-10-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .34214  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Oct-18 08:07:20  

Additional Information
 Earth MOID = .000363599 au 
 Jupiter MOID = 2.33882 au 
 T_jup = 3.708 
[ 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 27.501   .2671 3 autocmod 2.8

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