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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 ]

[ show orbit diagram ]
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 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456501.5 (2013-Jul-28.0) TDB
Reference: JPL 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1174979661675216 3.5379e-08  
q 1.99326219428151 7.9213e-08 au
tp 2455942.481940125555
(2012-Jan-15.98194013)
7.3261e-05 TDB
node 228.8304362460343 9.6353e-05 deg
peri 204.3645356831674 9.8857e-05 deg
i 2.6255163996401 4.5138e-06 deg
  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
 Jupiter MOID = 2.70083 au 
 T_jup = 3.611 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.251671440586238E-15 -2.788050727723821E-15 -4.365406349269394E-13 7.265491972427048E-15 -1.427091122710952E-13 -2.443985692280442E-16
q -2.788050727723821E-15 6.274638189047655E-15 1.047606524710869E-12 -1.655521632865768E-14 3.450622673880268E-13 5.413268166841983E-16
tp -4.365406349269394E-13 1.047606524710869E-12 5.367125913841665E-9 -5.582479177578156E-12 1.636232618781444E-9 -5.716041691315158E-13
node 7.265491972427048E-15 -1.655521632865768E-14 -5.582479177578156E-12 9.283904188400425E-9 -9.275430774632594E-9 -1.199545960022178E-10
peri -1.427091122710952E-13 3.450622673880268E-13 1.636232618781444E-9 -9.275430774632594E-9 9.772614559146589E-9 1.19655177947857E-10
i -2.443985692280442E-16 5.413268166841983E-16 -5.716041691315158E-13 -1.199545960022178E-10 1.19655177947857E-10 2.037481862921176E-11

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

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2024-May-23 06:31 < 00:01 Iris 0.044997069589424 0.0449955274564765 0.0449986117455187 3.15765346272549 3.15765342226563 2460453.771833077 0.444211503307243 104.494392837887 53.4527397513791 52.0542294396018 106824.742287527 T 27 CATAB v2.0f-lin.ifort 2020-Feb-23 02:53:41 2020-Feb-23 02:53

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