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(2013 NC15)
Classification: Apollo [NEO]          SPK-ID: 3645041
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 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2080592649344293 1.1247e-06  
a 1.140635081517331 1.081e-06 au
q .9033153848984126 4.4666e-07 au
i 20.9364079201865 0.00014787 deg
node 296.8060226482203 1.6675e-05 deg
peri 143.7099784137127 7.4095e-05 deg
M 102.6959122064317 0.0027639 deg
tp 2458873.568570811556
(2020-Jan-25.06857081)
0.0032358 TDB
period 444.9574820075256
1.22
0.00063254
1.732e-06
d
yr
n .8090660671122535 1.1501e-06 deg/d
Q 1.37795477813625 1.3059e-06 au
  Orbit Determination Parameters
   # obs. used (total)      46  
   data-arc span      199 days  
   first obs. used      2013-07-13  
   last obs. used      2014-01-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .30076  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:45:24  

Additional Information
 Earth MOID = .0472838 au 
 Jupiter MOID = 3.80891 au 
 T_jup = 5.417 
[ 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 22.1   n/a MPO283485  

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