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6586 Seydler (1984 UK1)
Classification: Main-belt Asteroid          SPK-ID: 2006586
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 30 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1535129414371406 3.3559e-08  
a 2.44625990261998 7.8566e-09 au
q 2.070727349449053 8.1948e-08 au
i 3.62596775176107 3.7561e-06 deg
node 228.2520932924004 5.8075e-05 deg
peri 244.881251793747 5.9281e-05 deg
M 46.04646135603183 1.1979e-05 deg
tp 2458821.749987138867
(2019-Dec-04.24998714)
4.6357e-05 TDB
period 1397.501626291164
3.83
6.7325e-06
1.843e-08
d
yr
n .2576025624781602 1.241e-09 deg/d
Q 2.821792455790906 9.0627e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1951  
   data-arc span      12855 days (35.20 yr)  
   first obs. used      1984-10-26  
   last obs. used      2020-01-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .46966  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jan-28 20:29:56  

Additional Information
 Earth MOID = 1.09034 au 
 Jupiter MOID = 2.29413 au 
 T_jup = 3.479 
[ 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 13.7   n/a MPO452260  
diameter diameter 5.312 km 0.189 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.172   0.018 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

6586 Seydler (1984 UK1)          Discovered 1984-Oct-28 by Mrkos, A. at Klet
Reference: DISCOVERY.DBLast Updated: 2003-08-29

Alternate Designations
 1984 UK1 = 1992 YO 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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