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434192 (2003 CQ1)
Classification: Main-belt Asteroid          SPK-ID: 2434192
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 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2144448439881171 1.1788e-07  
a 3.176710280049944 6.3733e-08 au
q 2.495481139649186 3.9768e-07 au
i 28.74727552850466 1.2971e-05 deg
node 130.191003927826 1.8713e-05 deg
peri 316.6031487352611 3.4962e-05 deg
M 348.420097112448 3.8589e-05 deg
tp 2458667.022299931963
(2019-Jul-02.52229993)
0.00022303 TDB
period 2068.068118364789
5.66
6.2236e-05
1.704e-07
d
yr
n .1740755039948346 5.2386e-09 deg/d
Q 3.857939420450701 7.74e-08 au
  Orbit Determination Parameters
   # obs. used (total)      109  
   data-arc span      5866 days (16.06 yr)  
   first obs. used      2002-12-14  
   last obs. used      2019-01-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5658  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 05:34:13  

Additional Information
 Earth MOID = 1.56846 au 
 Jupiter MOID = 1.47184 au 
 T_jup = 2.976 
[ 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 15.5   n/a MPO419178  
diameter diameter 4.853 km 0.513 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.039   0.024 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

434192 (2003 CQ1)          Discovered 2003-Feb-02 by NEAT at Palomar
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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