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(2014 EB25)
Classification: Apollo [NEO]          SPK-ID: 3663826
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 2456728.5 (2014-Mar-12.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4204479617338608 0.023297  
a 1.377852146972951 0.040941 au
q .7985370202075495 0.0089481 au
i 10.9695621102443 0.5179 deg
node 352.6349148178466 0.010139 deg
peri 252.0774299428981 0.55591 deg
M 327.8026216116814 1.8814 deg
tp 2456781.334835979863
(2014-May-03.83483598)
0.7454 TDB
period 590.7481262403485
1.62
26.33
0.07209
d
yr
n .6093967699755892 0.027161 deg/d
Q 1.957167273738352 0.058155 au
  Orbit Determination Parameters
   # obs. used (total)      12  
   first obs. used      2014-03-12  
   last obs. used      2014-03-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .49377  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:42:05  

Additional Information
 Earth MOID = .00477762 au 
 Jupiter MOID = 3.11856 au 
 T_jup = 4.693 
[ 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 27.1   n/a MPO286775  

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