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JPL Small-Body Database Browser
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160928 (2001 XZ200)
Classification: Main-belt Asteroid          SPK-ID: 2160928
[ 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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09732602138763569 5.5522e-08  
a 2.65111531824495 2.4447e-08 au
q 2.393092812080354 1.5046e-07 au
i 24.05867973688015 6.0769e-06 deg
node 79.04591894210269 1.3928e-05 deg
peri 202.5631803215578 4.0846e-05 deg
M 254.2161757228089 4.3366e-05 deg
tp 2459463.795538753151
(2021-Sep-06.29553875)		 0.0001923 TDB
period 1576.672001515987
4.32		 2.1808e-05
5.971e-08		 d
yr
n .2283290371452377 3.1582e-09 deg/d
Q 2.909137824409547 2.6826e-08 au
   Orbit Determination Parameters
   # obs. used (total)      596  
   data-arc span      7686 days (21.04 yr)  
   first obs. used      1999-04-10  
   last obs. used      2020-04-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54003  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-21 01:36:56  

Additional Information
 Earth MOID = 1.38659 au 
 Jupiter MOID = 2.20353 au 
 T_jup = 3.260 
[ 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 15.2   n/a MPO502933  
diameter diameter 5.844 km 0.274 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.062   0.008 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

160928 (2001 XZ200)          Discovered 2001-Dec-15 by LINEAR at Socorro
Reference: 20070828/Numbers.arcLast Updated: 2007-08-30
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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