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(2016 TD)
Classification: Apollo [NEO]          SPK-ID: 3760082
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 .4696927866885257 0.00027334  
a 1.611260313324019 0.00073411 au
q .8544629666782333 5.1125e-05 au
i 13.42270494977189 0.0055754 deg
node 8.034778650726896 6.1167e-05 deg
peri 302.4139249121196 0.0014176 deg
M 305.3816528436007 0.45241 deg
tp 2459113.839957358006
(2020-Sep-21.33995736)
1.0163 TDB
period 747.0453935935599
2.05
0.51054
0.001398
d
yr
n .4818984269058526 0.00032934 deg/d
Q 2.368057659969804 0.0010789 au
  Orbit Determination Parameters
   # obs. used (total)      35  
   data-arc span      3 days  
   first obs. used      2016-10-01  
   last obs. used      2016-10-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .32176  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:23:30  

Additional Information
 Earth MOID = .00154289 au 
 Jupiter MOID = 3.01399 au 
 T_jup = 4.185 
[ 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 28.1   n/a E2016T36  

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