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JPL Small-Body Database Browser
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(2016 TC)
Classification: Apollo [NEO]          SPK-ID: 3760081
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 2457663.5 (2016-Oct-02.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4043011816618174 0.0010504  
a 1.32145599649905 0.0016706 au
q .7871897756003895 0.00039334 au
i 1.642429348444933 0.0040038 deg
node 211.5942702499981 0.0069767 deg
peri 237.1328286641435 0.00318 deg
M 321.6608451346742 0.098886 deg
tp 2457722.590480344036
(2016-Nov-30.09048034)
0.040366 TDB
period 554.8524217233605
1.52
1.0522
0.002881
d
yr
n .6488211746140482 0.0012304 deg/d
Q 1.85572221739771 0.0023461 au
  Orbit Determination Parameters
   # obs. used (total)      23  
   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      8  
   norm. resid. RMS      .55851  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:23:30  

Additional Information
 Earth MOID = .00867534 au 
 Jupiter MOID = 3.37235 au 
 T_jup = 4.859 
[ 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 25.9   n/a E2016T29  

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