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JPL Small-Body Database Browser
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(2013 CY32)
Classification: Apollo [NEO]          SPK-ID: 3626031
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | 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 2456330.5 (2013-Feb-07.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .8684052382759989 0.0013385  
a 2.030541258834549 0.015948 au
q .2672085931270857 0.00061921 au
i 17.92159149466089 0.058031 deg
node 136.806810593451 0.00054642 deg
peri 235.4104912519074 0.0041376 deg
M 14.0480161039883 0.18743 deg
tp 2456289.259051019098
(2012-Dec-27.75905102)
0.064358 TDB
period 1056.85682043813
2.89
12.451
0.03409
d
yr
n .3406327073243077 0.0040131 deg/d
Q 3.793873924542013 0.029798 au
  Orbit Determination Parameters
   # obs. used (total)      19  
   data-arc span      1 day  
   first obs. used      2013-02-06  
   last obs. used      2013-02-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .41577  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:46:55  

Additional Information
 Earth MOID = .000317856 au 
 Jupiter MOID = 1.97275 au 
 T_jup = 3.152 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 28.1   n/a MPO253310  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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