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(2020 TM6)
Classification: Apollo [NEO]          SPK-ID: 54068387
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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2037774287205814 0.00028717  
a 1.198163313076738 0.0004201 au
q .9540046739506272 9.6237e-06 au
i 14.06922788417699 0.015925 deg
node 205.617097532599 0.00012466 deg
peri 233.2634139148623 0.017156 deg
M 217.8981635285126 0.090277 deg
tp 2459189.590470828338
(2020-Dec-06.09047083)
0.020681 TDB
period 479.0407442190963
1.31
0.25194
0.0006898
d
yr
n .7515018385061392 0.00039524 deg/d
Q 1.442321952202848 0.00050571 au
  Orbit Determination Parameters
   # obs. used (total)      37  
   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      .52653  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Oct-27 07:15:16  

Additional Information
 Earth MOID = .0248819 au 
 Jupiter MOID = 3.80756 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 26.125   .3666 8 autocmod 2.8

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