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97478 (2000 CP53)
Classification: Main-belt Asteroid          SPK-ID: 2097478
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .02263084292020844 3.8052e-08  
a 2.972897048469764 2.0809e-08 au
q 2.905617882347893 1.1609e-07 au
i 8.951347280276819 4.7632e-06 deg
node 330.737489406287 2.5608e-05 deg
peri 130.9885366571794 0.00010651 deg
M 326.8587749698709 0.00010291 deg
tp 2458772.859128089986
(2019-Oct-16.35912809)
0.00053543 TDB
period 1872.268935622786
5.13
1.9658e-05
5.382e-08
d
yr
n .1922800689315772 2.0188e-09 deg/d
Q 3.040176214591634 2.128e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1297  
   data-arc span      7378 days (20.20 yr)  
   first obs. used      1998-11-16  
   last obs. used      2019-01-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53531  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 07:02:01  

Additional Information
 Earth MOID = 1.9299 au 
 Jupiter MOID = 1.99281 au 
 T_jup = 3.243 
[ 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 13.9   n/a MPO337971  
diameter diameter 6.213 km 0.179 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.182   0.027 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

97478 (2000 CP53)          Discovered 2000-Feb-02 by LINEAR at Socorro
Reference: 20050224/Numbers.arcLast Updated: 2005-02-28

Alternate Designations
 2000 CP53 = 2002 PV113 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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