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JPL Small-Body Database Browser
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32825 (1992 CK3)
Classification: Main-belt Asteroid          SPK-ID: 2032825
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .11786842281108 3.542e-08  
a 2.25838471721846 9.0812e-09 au
q 1.992192472499273 7.9335e-08 au
i 2.627388469763582 4.5159e-06 deg
node 228.7555338717584 9.6255e-05 deg
peri 204.3471214056962 9.8745e-05 deg
M 168.0866761419068 2.2403e-05 deg
tp 2458421.703222238523
(2018-Oct-30.20322224)
7.5979e-05 TDB
period 1239.639243137977
3.39
7.4771e-06
2.047e-08
d
yr
n .2904070696315721 1.7516e-09 deg/d
Q 2.524576961937647 1.0152e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1058  
   data-arc span      24271 days (66.45 yr)  
   first obs. used      1953-08-16  
   last obs. used      2020-01-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53617  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 02:53:28  

Additional Information
 Earth MOID = 1.00725 au 
 Jupiter MOID = 2.70083 au 
 T_jup = 3.611 
[ 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 15.1   n/a MPO474180  

32825 (1992 CK3)          Discovered 1992-Feb-02 by Elst, E. W. at La Silla
Reference: 20020128/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 1992 CK3 = 1999 FC21 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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