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JPL Small-Body Database Browser
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413907 (2006 WO29)
Classification: Mars-crossing Asteroid          SPK-ID: 2413907
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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .370962747226677 8.7477e-08  
a 2.569184435758512 3.1275e-08 au
q 1.616112719337515 2.2856e-07 au
i 28.30408129692306 1.089e-05 deg
node 116.4650772689407 1.5195e-05 deg
peri 254.5671427151836 2.8237e-05 deg
M 66.45155551188478 2.0479e-05 deg
tp 2458322.852350546268
(2018-Jul-23.35235055)
8.8196e-05 TDB
period 1504.150700963908
4.12
2.7465e-05
7.52e-08
d
yr
n .239337720461986 4.3702e-09 deg/d
Q 3.52225615217951 4.2877e-08 au
  Orbit Determination Parameters
   # obs. used (total)      303  
   data-arc span      5429 days (14.86 yr)  
   first obs. used      2004-04-25  
   last obs. used      2019-03-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .48301  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-14 08:35:00  

Additional Information
 Earth MOID = .796329 au 
 Jupiter MOID = 2.50682 au 
 T_jup = 3.174 
[ 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 16.2   n/a MPO382580  
diameter diameter 3.380 km 0.980 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2015ApJ...814..117N)  
geometric albedo albedo 0.056   0.030 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2015ApJ...814..117N)  

413907 (2006 WO29)          Discovered 2006-Nov-22 by Mt. Lemmon Survey at Mount Lemmon
Reference: Last Updated: 2014-11-10
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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