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71362 (2000 AB133)
Classification: Main-belt Asteroid          SPK-ID: 2071362
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 28 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1027799431125827 4.9899e-08  
a 2.938268740145804 1.942e-08 au
q 2.636273646184138 1.4899e-07 au
i 16.41363782459341 5.4056e-06 deg
node 322.0312062908447 1.7626e-05 deg
peri 142.429007867252 3.6515e-05 deg
M 30.21897165371272 2.8278e-05 deg
tp 2458846.076682047032
(2019-Dec-28.57668205)
0.00014451 TDB
period 1839.652093397375
5.04
1.8238e-05
4.993e-08
d
yr
n .1956891747586743 1.94e-09 deg/d
Q 3.24026383410747 2.1416e-08 au
  Orbit Determination Parameters
   # obs. used (total)      863  
   data-arc span      7807 days (21.37 yr)  
   first obs. used      1998-09-19  
   last obs. used      2020-02-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .46159  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 16:25:16  

Additional Information
 Earth MOID = 1.66958 au 
 Jupiter MOID = 1.87206 au 
 T_jup = 3.205 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 14.3   n/a MPO449450  
diameter diameter 6.291 km 0.124 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.102   0.025 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

71362 (2000 AB133)          Discovered 2000-Jan-03 by LINEAR at Socorro
Reference: 20031109/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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