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(2017 TA6)
Classification: Apollo [NEO]          SPK-ID: 3785931
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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1710642915135832 3.6303e-06  
a 1.119128794182376 3.3422e-06 au
q .9276858198931174 1.2933e-06 au
i .9912146180531396 2.1976e-05 deg
node 37.26463447181345 9.9846e-05 deg
peri 49.60055153999484 0.0001186 deg
M 197.0938777482326 0.0040207 deg
tp 2459396.183152793008
(2021-Jun-30.68315279)
0.0057063 TDB
period 432.4327043805665
1.18
0.0019371
5.303e-06
d
yr
n .8324994764576793 3.7293e-06 deg/d
Q 1.310571768471635 3.9139e-06 au
  Orbit Determination Parameters
   # obs. used (total)      43  
   data-arc span      207 days  
   first obs. used      2017-09-30  
   last obs. used      2018-04-25  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      4  
   norm. resid. RMS      .41106  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 19:53:24  

Additional Information
 Earth MOID = .00238121 au 
 Jupiter MOID = 3.82584 au 
 T_jup = 5.563 
[ 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 27.1   n/a E2018L02  

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