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(2018 LE4)
Classification: Apollo [NEO]          SPK-ID: 3825166
[ 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.


Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2750160328570188 0.00021428  
a 1.251248621764503 0.00036233 au
q .907135189689017 5.7422e-06 au
i 20.99182963310046 0.010905 deg
node 256.3131419018852 0.0010816 deg
peri 295.0656927780138 0.017794 deg
M 187.1066968101905 0.25114 deg
tp 2459246.021492811239
(2021-Jan-31.52149281)		 0.46328 TDB
period 511.2270734686015
1.40		 0.22206
0.000608		 d
yr
n .7041880578770061 0.00030587 deg/d
Q 1.595362053839989 0.00046198 au
   Orbit Determination Parameters
   # obs. used (total)      54  
   data-arc span      23 days  
   first obs. used      2018-06-11  
   last obs. used      2018-07-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .35359  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Dec-29 06:53:49  

Additional Information
 Earth MOID = .0180544 au 
 Jupiter MOID = 3.48778 au 
 T_jup = 5.039 
[ 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 23.8   n/a E2018N16  

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