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JPL Small-Body Database Browser
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(2018 LX5)
Classification: Apollo [NEO]          SPK-ID: 3825245
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3100872515469263 0.00030437  
a 1.016996256295258 0.00018552 au
q .7016386823471479 0.00018155 au
i 15.11176384566712 0.017116 deg
node 88.58280477792053 0.0005518 deg
peri 289.8796289684511 0.013567 deg
M 223.9832422461041 0.030099 deg
tp 2458742.036149282274
(2019-Sep-15.53614928)
0.070048 TDB
period 374.6083540221656
1.03
0.1025
0.0002806
d
yr
n .961003661916997 0.00026295 deg/d
Q 1.332353830243368 0.00024304 au
  Orbit Determination Parameters
   # obs. used (total)      60  
   data-arc span      7 days  
   first obs. used      2018-06-14  
   last obs. used      2018-06-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .4557  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Jun-21 06:27:53  

Additional Information
 Earth MOID = .00690745 au 
 Jupiter MOID = 4.15684 au 
 T_jup = 5.928 
[ 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 25.2   n/a MPO451977  

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