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134672 (1999 VE205)
Classification: Main-belt Asteroid          SPK-ID: 2134672
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2483939027099909 4.8225e-08  
a 2.336478984311157 1.0353e-08 au
q 1.756111850798233 1.1072e-07 au
i 3.60767071564434 5.5592e-06 deg
node 273.9008104938123 8.5164e-05 deg
peri 91.48086772054471 8.6008e-05 deg
M 347.7765100282252 1.346e-05 deg
tp 2459244.792884639510
(2021-Jan-30.29288464)
4.8969e-05 TDB
period 1304.49147559684
3.57
8.67e-06
2.374e-08
d
yr
n .2759696071109167 1.8342e-09 deg/d
Q 2.916846117824081 1.2924e-08 au
  Orbit Determination Parameters
   # obs. used (total)      417  
   data-arc span      8614 days (23.58 yr)  
   first obs. used      1997-01-11  
   last obs. used      2020-08-12  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .56829  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 18:09:24  

Additional Information
 Earth MOID = .757445 au 
 Jupiter MOID = 2.56638 au 
 T_jup = 3.523 
[ 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 16.3   n/a MPO436658  
diameter diameter 3.887 km 0.806 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2012ApJ...759L...8M)  
geometric albedo albedo 0.035   0.034 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2012ApJ...759L...8M)  

134672 (1999 VE205)          Discovered 1999-Nov-11 by CSS at Catalina
Reference: 20060907/Numbers.arcLast Updated: 2006-09-10

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