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JPL Small-Body Database Browser
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65194 (2002 CV264)
Classification: Jupiter Trojan          SPK-ID: 2065194
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 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .01521863041190683 9.3689e-08  
a 5.136019455263753 1.8139e-07 au
q 5.057856273385731 4.0264e-07 au
i 17.11352725347625 7.3223e-06 deg
node 75.53346766840741 2.8734e-05 deg
peri 133.8339641085772 0.00031736 deg
M 155.0315077051001 0.00030943 deg
tp 2457169.636835966174
(2015-May-27.13683597)
0.0036693 TDB
period 4251.463130358852
11.64
0.00022523
6.166e-07
d
yr
n .08467673103626647 4.4859e-09 deg/d
Q 5.214182637141775 1.8415e-07 au
  Orbit Determination Parameters
   # obs. used (total)      368  
   data-arc span      10861 days (29.74 yr)  
   first obs. used      1990-01-01  
   last obs. used      2019-09-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57083  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 07:38:39  

Additional Information
 Earth MOID = 4.06004 au 
 Jupiter MOID = .113798 au 
 T_jup = 2.912 
[ 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 12.2   n/a MPO453046  
diameter diameter 18.553 km 0.748 urn:nasa:pds:neowise_diameters_albedos::2.0[jupiter_trojans] (http://adsabs.harvard.edu/abs/2011ApJ...742...40G)  
geometric albedo albedo 0.081   0.017 urn:nasa:pds:neowise_diameters_albedos::2.0[jupiter_trojans] (http://adsabs.harvard.edu/abs/2011ApJ...742...40G)  

65194 (2002 CV264)          Discovered 2002-Feb-08 by LINEAR at Socorro
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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