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(2013 LR6)
Classification: Apollo [NEO]          SPK-ID: 3639547
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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5218809038161129 9.1717e-05  
a 2.015056125092568 0.00037402 au
q .9634368132890643 6.0343e-06 au
i 2.524762720858704 0.00082956 deg
node 76.37764030003764 5.9032e-05 deg
peri 213.5097178244426 0.0010147 deg
M 149.1892278817625 0.24274 deg
tp 2458567.523711924873
(2019-Mar-25.02371192)
0.58393 TDB
period 1044.790337212409
2.86
0.29089
0.0007964
d
yr
n .3445667395436594 9.5934e-05 deg/d
Q 3.066675436896071 0.00056921 au
  Orbit Determination Parameters
   # obs. used (total)      61  
   data-arc span      1 day  
   first obs. used      2013-06-06  
   last obs. used      2013-06-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .36113  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:45:39  

Additional Information
 Earth MOID = .00148851 au 
 Jupiter MOID = 2.14861 au 
 T_jup = 3.643 
[ 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 27.8   n/a MPO263326  

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