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(2016 TD11)
Classification: Apollo [NEO]          SPK-ID: 3760497
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 .4548321166099414 0.00033623  
a 1.80306120354886 0.0010902 au
q .9829710599614634 1.1905e-05 au
i 4.632344718054283 0.0025264 deg
node 10.97822581657719 0.0015682 deg
peri 30.62595219094916 0.0029669 deg
M 172.2880572539649 0.48673 deg
tp 2458577.279395555553
(2019-Apr-03.77939556)
0.81179 TDB
period 884.3295352469638
2.42
0.80206
0.002196
d
yr
n .4070880657621189 0.00036921 deg/d
Q 2.623151347136256 0.0015861 au
  Orbit Determination Parameters
   # obs. used (total)      64  
   data-arc span      7 days  
   first obs. used      2016-10-06  
   last obs. used      2016-10-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .44312  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Feb-10 07:08:19  

Additional Information
 Earth MOID = .0149434 au 
 Jupiter MOID = 2.80919 au 
 T_jup = 3.931 
[ 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 26.3   n/a E2016U05  

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