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351555 (2005 TK134)
Classification: Main-belt Asteroid          SPK-ID: 2351555
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 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1049188677632515 1.0757e-07  
a 3.115106548735126 5.5144e-08 au
q 2.788273096679946 3.2391e-07 au
i 14.61670138983242 1.3137e-05 deg
node 337.4270114423588 2.8281e-05 deg
peri 49.97208834343237 5.9109e-05 deg
M 167.8374638342907 5.4125e-05 deg
tp 2457664.244907033222
(2016-Oct-02.74490703)
0.00029097 TDB
period 2008.203804847875
5.50
5.3324e-05
1.46e-07
d
yr
n .1792646738000134 4.76e-09 deg/d
Q 3.441940000790305 6.0929e-08 au
  Orbit Determination Parameters
   # obs. used (total)      170  
   data-arc span      6270 days (17.17 yr)  
   first obs. used      2002-03-09  
   last obs. used      2019-05-09  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .62574  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 09:27:04  

Additional Information
 Earth MOID = 1.81318 au 
 Jupiter MOID = 2.09616 au 
 T_jup = 3.159 
[ 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 15.7   n/a MPO437487  
diameter diameter 4.348 km 0.174 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.045   0.007 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

351555 (2005 TK134)          Discovered 2005-Oct-10 by CSS at Catalina
Reference: 20130127/Numbers.arcLast Updated: 2013-01-31

Alternate Designations
 2005 TK134 = 2002 EP35 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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