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(2018 LV3)
Classification: Apollo [NEO]          SPK-ID: 3825156
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5255991400333668 0.00033887  
a 2.002165518699203 0.001381 au
q .9498290438664422 2.3313e-05 au
i 8.996787509033092 0.0044614 deg
node 83.08497197632755 1.679e-05 deg
peri 216.6208731610364 0.0010404 deg
M 239.0178665687474 0.24569 deg
tp 2459348.249994126814
(2021-May-13.74999413)
1.066 TDB
period 1034.780874952842
2.83
1.0707
0.002931
d
yr
n .3478997425579655 0.00035996 deg/d
Q 3.054501993531964 0.0021069 au
  Orbit Determination Parameters
   # obs. used (total)      38  
   data-arc span      3 days  
   first obs. used      2018-06-11  
   last obs. used      2018-06-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .25886  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Jun-26 06:22:07  

Additional Information
 Earth MOID = .00206287 au 
 Jupiter MOID = 2.22325 au 
 T_jup = 3.641 
[ 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 26.5   n/a E2018M99  

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