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103326 (2000 AD67)
Classification: Main-belt Asteroid          SPK-ID: 2103326
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 .1648493961634172 5.3608e-08  
a 2.851665894202037 1.7455e-08 au
q 2.38157049348302 1.4668e-07 au
i 6.627049416243332 3.441e-06 deg
node 111.6489908571592 4.301e-05 deg
peri 94.35482453287074 4.478e-05 deg
M 62.79038465890951 1.0279e-05 deg
tp 2458893.712943921662
(2020-Feb-14.21294392)
5.0548e-05 TDB
period 1758.921223180156
4.82
1.6149e-05
4.421e-08
d
yr
n .2046709058118672 1.8792e-09 deg/d
Q 3.321761294921053 2.0332e-08 au
  Orbit Determination Parameters
   # obs. used (total)      798  
   data-arc span      7501 days (20.54 yr)  
   first obs. used      2000-01-04  
   last obs. used      2020-07-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .4904  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 19:49:24  

Additional Information
 Earth MOID = 1.38787 au 
 Jupiter MOID = 1.67953 au 
 T_jup = 3.275 
[ 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 15.10   n/a E2021B55  
diameter diameter 6.084 km 0.061 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.053   0.005 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

103326 (2000 AD67)          Discovered 2000-Jan-04 by LINEAR at Socorro
Reference: 20051019/Numbers.arcLast Updated: 2005-10-26

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