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15119 (2000 DU97)
Classification: Main-belt Asteroid          SPK-ID: 2015119
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 31 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1125386697465515 4.5056e-08  
a 3.110091718521565 2.1073e-08 au
q 2.760086133729382 1.4207e-07 au
i 16.10190308732142 5.7563e-06 deg
node 349.9424775738007 1.5074e-05 deg
peri 31.34142356098199 2.8519e-05 deg
M 46.20341035112904 2.2681e-05 deg
tp 2458943.383614579873
(2020-Apr-03.88361458)
0.00012642 TDB
period 2003.356419965736
5.48
2.0361e-05
5.575e-08
d
yr
n .179698428303715 1.8263e-09 deg/d
Q 3.460097303313749 2.3444e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1528  
   data-arc span      10388 days (28.44 yr)  
   first obs. used      1992-10-01  
   last obs. used      2021-03-11  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .46548  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 00:48:38  

Additional Information
 Earth MOID = 1.7709 au 
 Jupiter MOID = 2.04415 au 
 T_jup = 3.149 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 13.62   n/a E2021B10  
diameter diameter 10.672 km 0.149 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.074   0.009 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

15119 (2000 DU97)          Discovered 2000-Feb-29 by LINEAR at Socorro
Reference: 20000523/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 DU97 = 1992 TQ1 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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