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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5060728449531053 0.00039208  
a 1.56541727617107 0.0010385 au
q .7732021016804357 0.00010085 au
i 2.667158973901776 0.0022691 deg
node 197.1049435694019 0.00039741 deg
peri 252.4629732589237 0.0016968 deg
M 283.5758626152888 0.64108 deg
tp 2459152.369881901331
(2020-Oct-29.86988190)
1.4251 TDB
period 715.3912278951888
1.96
0.71188
0.001949
d
yr
n .5032211550303538 0.00050075 deg/d
Q 2.357632450661705 0.001564 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 = .00143094 au 
 Jupiter MOID = 2.88084 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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