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(2016 SL2)
Classification: Apollo [NEO]          SPK-ID: 3759746
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 2457657.5 (2016-Sep-26.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7695813177198189 0.00098912  
a 2.06348442340905 0.0071725 au
q .4754653617475927 0.00038836 au
i 1.810777974349838 0.0024912 deg
node 17.57220312111035 0.0035674 deg
peri 90.90404236016559 0.0036437 deg
M 343.6220857381055 0.097885 deg
tp 2457706.755679156979
(2016-Nov-14.25567916)
0.03757 TDB
period 1082.680261537848
2.96
5.645
0.01546
d
yr
n .3325081400197072 0.0017337 deg/d
Q 3.651503485070507 0.012692 au
  Orbit Determination Parameters
   # obs. used (total)      26  
   data-arc span      3 days  
   first obs. used      2016-09-25  
   last obs. used      2016-09-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .43638  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:23:38  

Additional Information
 Earth MOID = .00607696 au 
 Jupiter MOID = 1.52542 au 
 T_jup = 3.325 
[ 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 25.4   n/a E2016T08  

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