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434333 (2004 KS5)
Classification: Main-belt Asteroid          SPK-ID: 2434333
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 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .248479165029956 1.3711e-07  
a 3.09361012169639 5.4852e-08 au
q 2.324912461729051 4.128e-07 au
i 30.47025963627021 1.2364e-05 deg
node 216.934761825579 1.2412e-05 deg
peri 351.8965525630593 2.4407e-05 deg
M 278.7818181268929 2.0078e-05 deg
tp 2459048.881369758890
(2020-Jul-18.38136976)
0.00011914 TDB
period 1987.452678581181
5.44
5.2858e-05
1.447e-07
d
yr
n .1811363882419579 4.8175e-09 deg/d
Q 3.86230778166373 6.8481e-08 au
  Orbit Determination Parameters
   # obs. used (total)      162  
   data-arc span      5380 days (14.73 yr)  
   first obs. used      2004-04-17  
   last obs. used      2019-01-09  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .58411  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 18:29:00  

Additional Information
 Earth MOID = 1.32146 au 
 Jupiter MOID = 1.1287 au 
 T_jup = 2.969 
[ 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 15.8   n/a MPO428051  
diameter diameter 3.532 km 0.153 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.107   0.014 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

434333 (2004 KS5)          Discovered 2004-May-17 by LINEAR at Socorro
Reference: Last Updated: 2015-06-04

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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