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233141 (2005 UG132)
Classification: Main-belt Asteroid          SPK-ID: 2233141
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 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1372902023762851 6.966e-08  
a 2.352120660132925 2.532e-08 au
q 2.029197538689834 1.6172e-07 au
i 13.2165163456927 8.0761e-06 deg
node 101.6200245262416 3.0075e-05 deg
peri 347.4735444944969 4.5443e-05 deg
M 343.6622559911932 4.4695e-05 deg
tp 2459060.296726259288
(2020-Jul-29.79672626)
0.00016432 TDB
period 1317.612850448616
3.61
2.1276e-05
5.825e-08
d
yr
n .2732213790093413 4.4118e-09 deg/d
Q 2.675043781576015 2.8796e-08 au
  Orbit Determination Parameters
   # obs. used (total)      154  
   data-arc span      5604 days (15.34 yr)  
   first obs. used      2003-03-09  
   last obs. used      2018-07-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .59564  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Oct-04 08:59:23  

Additional Information
 Earth MOID = 1.04758 au 
 Jupiter MOID = 2.5123 au 
 T_jup = 3.509 
[ 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 16.7   n/a MPO454686  
diameter diameter 1.841 km 0.512 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.099   0.077 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

233141 (2005 UG132)          Discovered 2005-Oct-24 by NEAT at Palomar
Reference: 20100228/Numbers.arcLast Updated: 2010-03-03

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