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JPL Small-Body Database Browser
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32223 (2000 OE23)
Classification: Main-belt Asteroid          SPK-ID: 2032223
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 28 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09052265578090103 3.4054e-08  
a 2.301998856962427 8.8315e-09 au
q 2.093615806825589 8.0795e-08 au
i 4.988454041320696 3.9975e-06 deg
node 336.7110725522403 4.3534e-05 deg
peri 79.56008116306796 4.9689e-05 deg
M 22.35575694430427 2.287e-05 deg
tp 2458521.278518308638
(2019-Feb-06.77851831)
8.1058e-05 TDB
period 1275.722109519374
3.49
7.3414e-06
2.01e-08
d
yr
n .2821931181671135 1.6239e-09 deg/d
Q 2.510381907099264 9.631e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1592  
   data-arc span      16730 days (45.80 yr)  
   first obs. used      1974-02-16  
   last obs. used      2019-12-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50145  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-14 02:23:38  

Additional Information
 Earth MOID = 1.11142 au 
 Jupiter MOID = 2.73758 au 
 T_jup = 3.580 
[ 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 14.4   n/a MPO452623  
diameter diameter 3.710 km 0.247 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.425   0.039 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

32223 (2000 OE23)          Discovered 2000-Jul-23 by LINEAR at Socorro
Reference: 20011130/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 OE23 = 1974 DN2 = 1995 AP3 = 2000 MT4 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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