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58484 (1996 TO3)
Classification: Main-belt Asteroid          SPK-ID: 2058484
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 28 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06506635686822217 3.6836e-08  
a 2.957644310617066 1.6356e-08 au
q 2.76520117041319 1.1302e-07 au
i 9.066605528450628 3.966e-06 deg
node 300.4705188982809 2.5429e-05 deg
peri 24.40707563513457 3.9701e-05 deg
M 262.9578439640042 3.1199e-05 deg
tp 2459501.312637308923
(2021-Oct-13.81263731)
0.00016235 TDB
period 1857.878645692254
5.09
1.5411e-05
4.219e-08
d
yr
n .1937693836110929 1.6073e-09 deg/d
Q 3.150087450820943 1.742e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1458  
   data-arc span      8663 days (23.72 yr)  
   first obs. used      1996-10-08  
   last obs. used      2020-06-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .49338  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 22:50:56  

Additional Information
 Earth MOID = 1.75505 au 
 Jupiter MOID = 2.1043 au 
 T_jup = 3.245 
[ 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 14.0   n/a MPO337720  
diameter diameter 6.019 km 0.273 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.147   0.019 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

58484 (1996 TO3)          Discovered 1996-Oct-08 by Offutt, W. at Cloudcroft
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1996 TO3 = 2001 OC20 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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