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(2016 LS)
Classification: Centaur          SPK-ID: 3723796
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6063458135669066 1.8361e-05  
a 13.32438061947473 0.00065581 au
q 5.245198212484203 2.4267e-05 au
i 114.3326621437463 5.3963e-05 deg
node 117.5188441775825 3.1285e-05 deg
peri 141.1748496166499 0.00092659 deg
M 39.25959197448599 0.0029366 deg
tp 2457063.131416513845
(2015-Feb-09.63141651)
0.0085559 TDB
period 17765.15381281283
48.64
1.3116
0.003591
d
yr
n .02026438970319276 1.4961e-06 deg/d
Q 21.40356302646526 0.0010535 au
  Orbit Determination Parameters
   # obs. used (total)      64  
   data-arc span      417 days (1.14 yr)  
   first obs. used      2015-05-15  
   last obs. used      2016-07-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .37736  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Dec-16 23:38:25  

Additional Information
 Earth MOID = 4.3837 au 
 Jupiter MOID = .577764 au 
 T_jup = -0.658 
[ 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 13.3   n/a MPO381209  

[ show close-approach data ]
Alternate Designations
 2016 LS = 2015 MJ116 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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