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(2020 TM6)
Classification: Apollo [NEO]          SPK-ID: 54068387
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .203765377857637 0.00028608  
a 1.198145669272162 0.00041849 au
q .9540050642444283 9.5823e-06 au
i 14.0685583338728 0.015865 deg
node 205.6171028134629 0.00012427 deg
peri 233.2641373292212 0.017094 deg
M 217.8943703989575 0.089936 deg
tp 2459189.591341394186
(2020-Dec-06.09134139)
0.020604 TDB
period 479.0301629359772
1.31
0.25097
0.0006871
d
yr
n .7515184384080514 0.00039374 deg/d
Q 1.442286274299895 0.00050376 au
  Orbit Determination Parameters
   # obs. used (total)      39  
   data-arc span      10 days  
   first obs. used      2020-10-11  
   last obs. used      2020-10-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .52415  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-18 05:28:16  

Additional Information
 Earth MOID = .0248807 au 
 Jupiter MOID = 3.80757 au 
 T_jup = 5.254 
[ 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 26.118   .3585 9 autocmod 2.8

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