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118670 (2000 KP55)
Classification: Main-belt Asteroid          SPK-ID: 2118670
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 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09619319656831121 5.6741e-08  
a 2.445122768185275 1.8395e-08 au
q 2.209918593111575 1.323e-07 au
i 14.81415699867276 5.8381e-06 deg
node 80.26135234274247 2.061e-05 deg
peri 96.29103915960415 4.0853e-05 deg
M 144.8451499768545 3.4746e-05 deg
tp 2458438.610536392425
(2018-Nov-16.11053639)
0.00013236 TDB
period 1396.527304718524
3.82
1.5759e-05
4.315e-08
d
yr
n .2577822852325536 2.909e-09 deg/d
Q 2.680326943258974 2.0165e-08 au
  Orbit Determination Parameters
   # obs. used (total)      506  
   data-arc span      6940 days (19.00 yr)  
   first obs. used      2000-05-11  
   last obs. used      2019-05-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .60043  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 06:55:59  

Additional Information
 Earth MOID = 1.26792 au 
 Jupiter MOID = 2.41292 au 
 T_jup = 3.447 
[ 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 15.4   n/a MPO236850  
diameter diameter 2.769 km 0.960 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.159   0.105 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

118670 (2000 KP55)          Discovered 2000-May-27 by LINEAR at Socorro
Reference: 20051116/Numbers.arcLast Updated: 2005-11-21

Alternate Designations
 2000 KP55 = 2003 AK75 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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