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(2006 YC13)
Classification: Apollo [NEO]          SPK-ID: 3364629
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3774850939355737 1.1429e-07  
a 1.462743727658916 1.7053e-08 au
q .910579774219919 1.6025e-07 au
i 25.2486410380698 4.5457e-05 deg
node 290.0013454255766 2.5686e-05 deg
peri 277.4572739320005 4.7903e-05 deg
M 160.8487484379755 6.276e-05 deg
tp 2458711.787239728118
(2019-Aug-16.28723973)
0.00010817 TDB
period 646.1759554066807
1.77
1.13e-05
3.094e-08
d
yr
n .5571237942046737 9.7425e-09 deg/d
Q 2.014907681097913 2.349e-08 au
  Orbit Determination Parameters
   # obs. used (total)      85  
   data-arc span      3550 days (9.72 yr)  
   first obs. used      2006-12-24  
   last obs. used      2016-09-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57495  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:07:16  

Additional Information
 Earth MOID = .135526 au 
 Jupiter MOID = 3.27826 au 
 T_jup = 4.445 
[ 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 20.4   n/a MPO281880  

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