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JPL Small-Body Database Browser
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(2016 TB19)
Classification: Apollo [NEO]          SPK-ID: 3760627
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5061255431779612 0.00039551  
a 1.5654272501093 0.0010322 au
q .7731245328421483 0.00010937 au
i 2.668101355342801 0.0022806 deg
node 197.1908123007886 6.3603e-05 deg
peri 252.3117139205314 0.002223 deg
M 82.45990168049758 0.44103 deg
tp 2458436.634294160676
(2018-Nov-14.13429416)
0.71435 TDB
period 715.3980649980409
1.96
0.70759
0.001937
d
yr
n .5032163457151451 0.00049773 deg/d
Q 2.357729967376451 0.0015547 au
  Orbit Determination Parameters
   # obs. used (total)      31  
   data-arc span      2 days  
   first obs. used      2016-10-09  
   last obs. used      2016-10-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .42858  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:23:10  

Additional Information
 Earth MOID = .00122142 au 
 Jupiter MOID = 2.88133 au 
 T_jup = 4.269 
[ 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 29.1   n/a E2016-TA5  

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