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JPL Small-Body Database Browser
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351917 (2006 SL382)
Classification: Main-belt Asteroid          SPK-ID: 2351917
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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 .1881165105868635 5.4208e-08  
a 3.014608701306199 4.2963e-08 au
q 2.447511031631681 1.6993e-07 au
i 11.03908335113529 1.1076e-05 deg
node 123.6773490085098 3.7008e-05 deg
peri 304.2311951372479 5.6811e-05 deg
M 120.7277587619882 3.5887e-05 deg
tp 2457959.364998584486
(2017-Jul-24.86499858)		 0.00019079 TDB
period 1911.810530373704
5.23		 4.087e-05
1.119e-07		 d
yr
n .1883031787305985 4.0255e-09 deg/d
Q 3.581706370980717 5.1045e-08 au
   Orbit Determination Parameters
   # obs. used (total)      128  
   data-arc span      6357 days (17.40 yr)  
   first obs. used      2001-12-11  
   last obs. used      2019-05-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .48667  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 09:27:11  

Additional Information
 Earth MOID = 1.48169 au 
 Jupiter MOID = 1.77512 au 
 T_jup = 3.194 
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[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.5   n/a MPO437488  

351917 (2006 SL382)          Discovered 2006-Sep-28 by Becker, A. C. at Apache Point
Reference: 20130127/Numbers.arcLast Updated: 2013-01-31

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[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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