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58582 (1997 SF3)
Classification: Main-belt Asteroid          SPK-ID: 2058582
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1289970168786312 3.4252e-08  
a 2.281257484080429 8.9515e-09 au
q 1.986982073902002 7.6749e-08 au
i 6.866326524728722 4.001e-06 deg
node 347.0010928043828 3.3929e-05 deg
peri 23.37813204687903 3.8472e-05 deg
M 79.93228010637937 1.7121e-05 deg
tp 2458321.065781227603
(2018-Jul-21.56578123)
5.9983e-05 TDB
period 1258.519319406159
3.45
7.4076e-06
2.028e-08
d
yr
n .2860504359757214 1.6837e-09 deg/d
Q 2.575532894258855 1.0106e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1121  
   data-arc span      7851 days (21.49 yr)  
   first obs. used      1997-09-25  
   last obs. used      2019-03-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54961  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 03:35:22  

Additional Information
 Earth MOID = .98699 au 
 Jupiter MOID = 2.88623 au 
 T_jup = 3.585 
[ 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 15.2   n/a MPO412560  
diameter diameter 2.247 km 0.470 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.350   0.163 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

58582 (1997 SF3)          Discovered 1997-Sep-25 by Klet at Klet
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1997 SF3 = 1999 CX45 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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