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(2013 NC24)
Classification: Aten [NEO]          SPK-ID: 3645191
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2456484.5 (2013-Jul-11.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2692299468243224 0.0019983  
a .9784584781108627 0.00054191 au
q .7150281540792677 0.0015593 au
i 10.14936674454627 0.096956 deg
node 109.3568636581418 0.0082847 deg
peri 307.6706970980657 0.06792 deg
M 260.3228610236558 0.3163 deg
tp 2456582.382508564701
(2013-Oct-16.88250856)
0.22929 TDB
period 353.5184039707956
0.97
0.29369
0.0008041
d
yr
n 1.018334536353417 0.00084599 deg/d
Q 1.241888802142458 0.00068781 au
  Orbit Determination Parameters
   # obs. used (total)      8  
   data-arc span      8 days  
   first obs. used      2013-07-06  
   last obs. used      2013-07-14  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .46547  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 08:17:35  

Additional Information
 Earth MOID = .037912 au 
 Jupiter MOID = 4.06672 au 
 T_jup = 6.140 
[ 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 25.3   n/a MPO267688  

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