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34329 (2000 QO206)
Classification: Main-belt Asteroid          SPK-ID: 2034329
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 31 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .104302198882993 4.1352e-08  
a 2.658450460858168 1.3322e-08 au
q 2.381168232169155 1.1157e-07 au
i 4.15685239669756 4.7079e-06 deg
node 9.603687009883126 5.2453e-05 deg
peri 7.306687771667762 5.6169e-05 deg
M 179.3190015839147 2.2183e-05 deg
tp 2458211.884886380818
(2018-Apr-03.38488638)
9.5221e-05 TDB
period 1583.2200625434
4.33
1.1901e-05
3.258e-08
d
yr
n .2273846880273041 1.7092e-09 deg/d
Q 2.935732689547181 1.4711e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1309  
   data-arc span      8100 days (22.18 yr)  
   first obs. used      1998-02-23  
   last obs. used      2020-04-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .49647  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 07:47:14  

Additional Information
 Earth MOID = 1.38256 au 
 Jupiter MOID = 2.52945 au 
 T_jup = 3.375 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 14.7   n/a MPO337542  
diameter diameter 6.337 km 0.121 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.070   0.012 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

34329 (2000 QO206)          Discovered 2000-Aug-31 by LINEAR at Socorro
Reference: 20020128/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 QO206 = 1998 DT25 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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