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JPL Small-Body Database Browser
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47572 (2000 AK167)
Classification: Main-belt Asteroid          SPK-ID: 2047572
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 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1333986087786695 3.993e-08  
a 2.304326990956051 9.4845e-09 au
q 1.996932976191376 9.426e-08 au
i 11.07446816836766 3.8366e-06 deg
node 162.5329918137073 2.0018e-05 deg
peri 230.4489539258424 2.3307e-05 deg
M 255.8705208195585 1.2577e-05 deg
tp 2458970.060701267063
(2020-Apr-30.56070127)
4.5099e-05 TDB
period 1277.657907282915
3.50
7.8882e-06
2.16e-08
d
yr
n .281765563338923 1.7396e-09 deg/d
Q 2.611721005720726 1.075e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1069  
   data-arc span      8340 days (22.83 yr)  
   first obs. used      1996-11-17  
   last obs. used      2019-09-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5479  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Sep-24 02:13:38  

Additional Information
 Earth MOID = 1.01848 au 
 Jupiter MOID = 2.87145 au 
 T_jup = 3.553 
[ 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 15.4   n/a MPO452819  
diameter diameter 3.953 km 0.065 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.086   0.015 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

47572 (2000 AK167)          Discovered 2000-Jan-08 by LINEAR at Socorro
Reference: 20020921/Numbers.arcLast Updated: 2004-04-19
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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