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58451 (1996 JF3)
Classification: Main-belt Asteroid          SPK-ID: 2058451
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 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1465188918728769 5.1015e-08  
a 2.312084974129309 8.9444e-09 au
q 1.973320845803954 1.2039e-07 au
i 7.291651843663162 4.2584e-06 deg
node 69.1811353040638 4.125e-05 deg
peri 306.0841114320962 4.3489e-05 deg
M 44.57969296152174 1.3164e-05 deg
tp 2458441.484783063908
(2018-Nov-18.98478306)
4.6966e-05 TDB
period 1284.11557581618
3.52
7.4515e-06
2.04e-08
d
yr
n .2803485969486703 1.6268e-09 deg/d
Q 2.650849102454665 1.0255e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2318  
   data-arc span      10359 days (28.36 yr)  
   first obs. used      1990-09-17  
   last obs. used      2019-01-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .38495  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 03:34:47  

Additional Information
 Earth MOID = .984747 au 
 Jupiter MOID = 2.81968 au 
 T_jup = 3.559 
[ 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 14.5   n/a MPO452962  
diameter diameter 3.503 km 0.416 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.440   0.064 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

58451 (1996 JF3)          Discovered 1996-May-09 by Spacewatch at Kitt Peak
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1996 JF3 = 1990 SN2 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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