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(2013 EA29)
Classification: Apollo [NEO]          SPK-ID: 3631865
[ 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.


Orbital Elements at Epoch 2456358.5 (2013-Mar-07.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5967982581262675 0.0013608  
a 2.054733692972559 0.0062981 au
q .8284722040931826 0.00025671 au
i 5.506774871568857 0.0098102 deg
node 169.9082050614107 0.00029817 deg
peri 61.30356471181753 0.0046072 deg
M 344.3089097910089 0.080027 deg
tp 2456405.390229563459
(2013-Apr-22.89022956)		 0.023558 TDB
period 1075.800496843277
2.95		 4.9463
0.01354		 d
yr
n .334634535916602 0.0015386 deg/d
Q 3.280995181851935 0.010057 au
   Orbit Determination Parameters
   # obs. used (total)      29  
   data-arc span      9 days  
   first obs. used      2013-03-05  
   last obs. used      2013-03-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .53199  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:46:31  

Additional Information
 Earth MOID = .00789749 au 
 Jupiter MOID = 1.7311 au 
 T_jup = 3.536 
[ 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 26.5   n/a MPO256840  

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