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(2016 KL)
Classification: Apollo [NEO]          SPK-ID: 3753591
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 .3825458764120984 0.00028523  
a 1.576001894544029 0.00067806 au
q .9731088685685558 3.0856e-05 au
i 9.176965159641105 0.0054665 deg
node 77.9510900727493 0.00059848 deg
peri 218.1812953525491 0.0024939 deg
M 346.8340055027525 0.48309 deg
tp 2459026.929241427687
(2020-Jun-26.42924143)
0.9868 TDB
period 722.6591896234181
1.98
0.46638
0.001277
d
yr
n .4981601357447597 0.00032149 deg/d
Q 2.178894920519502 0.00093745 au
  Orbit Determination Parameters
   # obs. used (total)      98  
   data-arc span      12 days  
   first obs. used      2016-05-27  
   last obs. used      2016-06-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .45142  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:25:45  

Additional Information
 Earth MOID = .0127485 au 
 Jupiter MOID = 3.05162 au 
 T_jup = 4.306 
[ 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 25.8   n/a MPO381200  

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