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JPL Small-Body Database Browser
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324212 (2006 BY23)
Classification: Main-belt Asteroid          SPK-ID: 2324212
[ 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1625829344443963 7.763e-08  
a 3.134238446087805 3.4937e-08 au
q 2.624664762274405 2.5331e-07 au
i 9.373980976471895 8.9091e-06 deg
node 319.1094053302922 2.9663e-05 deg
peri 205.1618879596686 3.3789e-05 deg
M 195.1810380298814 1.8524e-05 deg
tp 2459928.399949509577
(2022-Dec-14.89994951)		 0.00011516 TDB
period 2026.732712247086
5.55		 3.3887e-05
9.278e-08		 d
yr
n .1776257904284081 2.9699e-09 deg/d
Q 3.643812129901205 4.0617e-08 au
   Orbit Determination Parameters
   # obs. used (total)      260  
   data-arc span      5871 days (16.07 yr)  
   first obs. used      2003-09-30  
   last obs. used      2019-10-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .56872  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-08 09:09:21  

Additional Information
 Earth MOID = 1.63654 au 
 Jupiter MOID = 1.38994 au 
 T_jup = 3.171 
[ show covariance matrix ]

[ 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 15.5   n/a MPO418665  

324212 (2006 BY23)          Discovered 2006-Jan-23 by CSS at Catalina
Reference: 20120406/Numbers.arcLast Updated: 2012-04-09

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