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67206 (2000 DU15)
Classification: Main-belt Asteroid          SPK-ID: 2067206
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 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1794624216118624 4.8731e-08  
a 2.648632124474531 1.1949e-08 au
q 2.17330218945736 1.3333e-07 au
i 5.631567640702129 4.8164e-06 deg
node 163.4327963238069 4.2828e-05 deg
peri 324.5534507886712 4.5038e-05 deg
M 325.644688642999 1.2073e-05 deg
tp 2459350.752697684905
(2021-May-16.25269768)
5.2977e-05 TDB
period 1574.457311839873
4.31
1.0655e-05
2.917e-08
d
yr
n .2286502131831779 1.5473e-09 deg/d
Q 3.123962059491701 1.4094e-08 au
  Orbit Determination Parameters
   # obs. used (total)      692  
   data-arc span      10068 days (27.56 yr)  
   first obs. used      1993-08-13  
   last obs. used      2021-03-07  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .52502  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 12:28:20  

Additional Information
 Earth MOID = 1.19092 au 
 Jupiter MOID = 1.94346 au 
 T_jup = 3.362 
[ 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 15.7   n/a MPO493339  
diameter diameter 4.099 km 0.508 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.046   0.036 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

67206 (2000 DU15)          Discovered 2000-Feb-27 by CSS at Catalina
Reference: 20030910/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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