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(2020 TG6)
Classification: Apollo [NEO]          SPK-ID: 54065915
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 2459138.5 (2020-Oct-16.0) TDB
Reference: JPL 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6990498109468994 0.00088556  
a 2.238867486005757 0.0057757 au
q .6737875931782725 0.0002445 au
i .3137001607159236 0.00038959 deg
node 212.1919284861798 0.0054444 deg
peri 250.090496905566 0.0058507 deg
M 346.3861369891818 0.059566 deg
tp 2459184.772172075210
(2020-Dec-01.27217208)
0.023403 TDB
period 1223.604346087399
3.35
4.7349
0.01296
d
yr
n .2942127503478859 0.0011385 deg/d
Q 3.803947378833241 0.0098132 au
  Orbit Determination Parameters
   # obs. used (total)      23  
   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      8  
   norm. resid. RMS      .31913  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Oct-17 08:36:24  

Additional Information
 Earth MOID = .000746385 au 
 Jupiter MOID = 1.38941 au 
 T_jup = 3.262 
[ 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 29.062   .25999 2 autocmod 2.8

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