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JPL Small-Body Database Browser
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(2015 LH)
Classification: Apollo [NEO]          SPK-ID: 3720917
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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4816054279509545 0.00043199  
a 1.902036780350757 0.0015491 au
q .9860055427714748 1.8617e-05 au
i 3.934510390624681 0.0023584 deg
node 83.58677465860993 0.00092593 deg
peri 201.5992495091191 0.00021851 deg
M 164.2830441293273 0.63896 deg
tp 2458163.262871040018
(2018-Feb-13.76287104)
1.1664 TDB
period 958.1351944128852
2.62
1.1705
0.003205
d
yr
n .3757298574347815 0.00045902 deg/d
Q 2.818068017930038 0.0022952 au
  Orbit Determination Parameters
   # obs. used (total)      32  
   data-arc span      5 days  
   first obs. used      2015-06-06  
   last obs. used      2015-06-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .44428  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:33:13  

Additional Information
 Earth MOID = .00309782 au 
 Jupiter MOID = 2.37077 au 
 T_jup = 3.793 
[ 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 27.2   n/a E2015L29  

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