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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 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1178684045108326 3.5426e-08  
a 2.258384717428463 9.1748e-09 au
q 1.992192514013523 7.9376e-08 au
i 2.627391432011803 4.5159e-06 deg
node 228.7554999182208 9.8175e-05 deg
peri 204.3471502831823 0.00010073 deg
M 168.0866786124489 2.2665e-05 deg
tp 2458421.703213650622
(2018-Oct-30.20321365)
7.6972e-05 TDB
period 1239.639243310885
3.39
7.5541e-06
2.068e-08
d
yr
n .2904070695910655 1.7697e-09 deg/d
Q 2.524576920843403 1.0256e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1046  
   data-arc span      24020 days (65.76 yr)  
   first obs. used      1953-08-16  
   last obs. used      2019-05-22  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .538  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 01:33:45  

Additional Information
 Earth MOID = 1.00725 au 
 Jupiter MOID = 2.70083 au 
 T_jup = 3.611 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456351.5 (2013-Feb-28.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1175825503392821 3.5391e-08  
q 1.992829310845598 7.9259e-08 au
tp 2455942.381529829423
(2012-Jan-15.88152983)
7.464e-05 TDB
node 228.8305058672487 9.8272e-05 deg
peri 204.3142982073455 0.00010084 deg
i 2.625599992203713 4.5142e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      1046  
   data-arc span      24020 days (65.76 yr)  
   first obs. used      1953-08-16  
   last obs. used      2019-05-22  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .538  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 01:33:45  

Additional Information
 Jupiter MOID = 2.70083 au 
 T_jup = 3.611 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.252557042648035E-15 -2.790375233069276E-15 -4.279009104654782E-13 6.385873322273983E-15 -1.389774353780175E-13 -2.457625502567558E-16
q -2.790375233069276E-15 6.282042214381543E-15 1.010868577759379E-12 -1.444512800248147E-14 3.308478330625626E-13 5.481252616242148E-16
tp -4.279009104654782E-13 1.010868577759379E-12 5.571176161853001E-9 -5.444292442958229E-12 1.704194018376722E-9 -5.974530092851529E-13
node 6.385873322273983E-15 -1.444512800248147E-14 -5.444292442958229E-12 9.657441381599558E-9 -9.648560676559763E-9 -1.201165917523657E-10
peri -1.389774353780175E-13 3.308478330625626E-13 1.704194018376722E-9 -9.648560676559763E-9 1.016804479791794E-8 1.198086013643953E-10
i -2.457625502567558E-16 5.481252616242148E-16 -5.974530092851529E-13 -1.201165917523657E-10 1.198086013643953E-10 2.03782355346298E-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

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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 26 CATAB v2.0e-lin.ifort 2019-Jul-13 01:33:51 2019-Jul-13 01:33

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