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86492 (2000 DN15)
Classification: Main-belt Asteroid          SPK-ID: 2086492
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06548653539743925 3.9683e-08  
a 2.324685803987331 1.0454e-08 au
q 2.17245018479659 9.1073e-08 au
i 7.140687402434382 4.2698e-06 deg
node 137.9320283415281 3.2509e-05 deg
peri 55.26890088075886 4.5815e-05 deg
M 234.2949740322747 3.396e-05 deg
tp 2459452.558837117973
(2021-Aug-26.05883712)
0.00012323 TDB
period 1294.62748294769
3.54
8.7332e-06
2.391e-08
d
yr
n .2780722676922702 1.8758e-09 deg/d
Q 2.476921423178071 1.1139e-08 au
  Orbit Determination Parameters
   # obs. used (total)      781  
   data-arc span      9724 days (26.62 yr)  
   first obs. used      1993-03-17  
   last obs. used      2019-10-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55139  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 10:18:39  

Additional Information
 Earth MOID = 1.18203 au 
 Jupiter MOID = 2.49235 au 
 T_jup = 3.562 
[ 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 15.8   n/a MPO337908  
rotation period rot_per 5.466 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Waszczak, A.; Chang, C.-K.; Ofeck, E.O.; Laher, F.; et al. (2015) Astron. J. 150, A75.]

86492 (2000 DN15)          Discovered 2000-Feb-26 by CSS at Catalina
Reference: 20040830/Numbers.arcLast Updated: 2004-09-06

Alternate Designations
 2000 DN15 = 2001 PX20 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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