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58465 (1996 NY3)
Classification: Main-belt Asteroid          SPK-ID: 2058465
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06605638910873982 6.2996e-08  
a 2.512114714052004 1.1386e-08 au
q 2.346173487014795 1.587e-07 au
i 9.760961284612396 4.4342e-06 deg
node 146.8142985808193 2.4809e-05 deg
peri 212.3875562198991 3.6196e-05 deg
M 319.441624966947 2.7034e-05 deg
tp 2459164.345936015973
(2020-Nov-10.84593602)
0.00010954 TDB
period 1454.312134489626
3.98
9.8874e-06
2.707e-08
d
yr
n .2475397072350894 1.6829e-09 deg/d
Q 2.678055941089214 1.2138e-08 au
  Orbit Determination Parameters
   # obs. used (total)      996  
   data-arc span      10235 days (28.02 yr)  
   first obs. used      1992-07-26  
   last obs. used      2020-08-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .539  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-25 05:18:10  

Additional Information
 Earth MOID = 1.34587 au 
 Jupiter MOID = 2.62508 au 
 T_jup = 3.438 
[ 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 15.1   n/a MPO337719  
diameter diameter 2.784 km 0.648 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.250   0.145 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

58465 (1996 NY3)          Discovered 1996-Jul-14 by Elst, E. W. at La Silla
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1996 NY3 = 1992 OJ4 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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