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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 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5967198172386332 0.0013604  
a 2.054370345007904 0.0062939 au
q .8284868481943195 0.00025667 au
i 5.506210064635832 0.009808 deg
node 169.9082214716582 0.00029809 deg
peri 61.30332766839854 0.0046068 deg
M 344.3042877245834 0.080013 deg
tp 2456405.391601010399
(2013-Apr-22.89160101)
0.023553 TDB
period 1075.515151369299
2.94
4.9425
0.01353
d
yr
n .3347233179761937 0.0015382 deg/d
Q 3.280253841821488 0.01005 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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .53605  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 07:49:18  

Additional Information
 Earth MOID = .00789659 au 
 Jupiter MOID = 1.73182 au 
 T_jup = 3.537 
[ 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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