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(2016 TH10)
Classification: Aten [NEO]          SPK-ID: 3760437
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 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5160208340405474 0.00037772  
a .765586888699105 6.6914e-05 au
q .3705281038620851 0.00032156 au
i 1.391986829139675 0.0018015 deg
node 7.690999504771256 0.0057873 deg
peri 164.3111911374609 0.00062306 deg
M 41.14558088802374 0.30287 deg
tp 2458972.535255554881
(2020-May-03.03525556)
0.20218 TDB
period 244.6753158654105
0.67
0.032078
8.782e-05
d
yr
n 1.471337632595626 0.0001929 deg/d
Q 1.160645673536125 0.00010144 au
  Orbit Determination Parameters
   # obs. used (total)      90  
   data-arc span      15 days  
   first obs. used      2016-10-04  
   last obs. used      2016-10-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .48676  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Sep-11 07:37:06  

Additional Information
 Earth MOID = .00695291 au 
 Jupiter MOID = 3.80558 au 
 T_jup = 7.454 
[ 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 24.9   n/a E2016U17  

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