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35838 (1999 JN58)
Classification: Main-belt Asteroid          SPK-ID: 2035838
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1219018878425081 4.0314e-08  
a 2.338381601354169 1.2716e-08 au
q 2.053328469652909 9.0643e-08 au
i 7.289487447867146 4.3935e-06 deg
node 61.58603761248101 3.3694e-05 deg
peri 243.9168771559751 4.1128e-05 deg
M 154.1396674804149 2.8155e-05 deg
tp 2458041.279064354653
(2017-Oct-14.77906435)
9.9435e-05 TDB
period 1306.085189640784
3.58
1.0654e-05
2.917e-08
d
yr
n .2756328628908286 2.2483e-09 deg/d
Q 2.62343473305543 1.4266e-08 au
  Orbit Determination Parameters
   # obs. used (total)      925  
   data-arc span      10707 days (29.31 yr)  
   first obs. used      1989-10-03  
   last obs. used      2019-01-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .56077  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 01:48:58  

Additional Information
 Earth MOID = 1.04973 au 
 Jupiter MOID = 2.58065 au 
 T_jup = 3.545 
[ 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 15.0   n/a MPO417059  
diameter diameter 2.783 km 0.087 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.301   0.071 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

35838 (1999 JN58)          Discovered 1999-May-10 by LINEAR at Socorro
Reference: 20020227/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1999 JN58 = 1989 TM12 = 2000 UA9 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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