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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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5218484305687101 9.1504e-05  
a 2.01516464607811 0.00037512 au
q .963554138184698 5.0881e-06 au
i 2.524608635738589 0.00082905 deg
node 76.37300978635474 6.6104e-05 deg
peri 213.5250583783728 0.001015 deg
M 218.038132754618 0.26198 deg
tp 2459612.534358385629
(2022-Feb-02.03435839)
0.87542 TDB
period 1044.874739231438
2.86
0.29175
0.0007988
d
yr
n .3445389064193471 9.6202e-05 deg/d
Q 3.066775153971521 0.00057087 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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .36312  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 08:14:01  

Additional Information
 Earth MOID = .001177 au 
 Jupiter MOID = 2.14812 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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