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65832 (1996 XN5)
Classification: Main-belt Asteroid          SPK-ID: 2065832
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .17503033297806 3.023e-08  
a 2.373393904541049 7.2809e-09 au
q 1.957977979141131 7.1813e-08 au
i 3.134967410345924 3.6385e-06 deg
node 68.51720028132334 6.6185e-05 deg
peri 19.03128038699486 6.7261e-05 deg
M 46.42767137851488 1.0867e-05 deg
tp 2458428.262559994956
(2018-Nov-05.76256000)
4.02e-05 TDB
period 1335.528501877647
3.66
6.1455e-06
1.683e-08
d
yr
n .2695562090167815 1.2404e-09 deg/d
Q 2.788809829940967 8.5553e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1502  
   data-arc span      8202 days (22.46 yr)  
   first obs. used      1996-12-07  
   last obs. used      2019-05-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52671  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 04:34:34  

Additional Information
 Earth MOID = .974626 au 
 Jupiter MOID = 2.41838 au 
 T_jup = 3.520 
[ 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 15.0   n/a MPO337764  
diameter diameter 2.475 km 0.503 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.263   0.182 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

65832 (1996 XN5)          Discovered 1996-Dec-07 by Kobayashi, T. at Oizumi
Reference: 20030910/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1996 XN5 = 1999 RL157 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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