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JPL Small-Body Database Browser
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(2014 EZ24)
Classification: Apollo [NEO]          SPK-ID: 3663827
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 .1599829256528003 0.0013231  
a 1.020739232181584 0.002023 au
q .8574383834885817 0.0029025 au
i 32.81465091787323 0.2423 deg
node 352.8758915857953 0.0064709 deg
peri 39.02864067628272 0.35926 deg
M 125.6144641895393 0.42312 deg
tp 2456597.065981256610
(2013-Oct-31.56598126)
0.36237 TDB
period 376.6783312168974
1.03
1.1198
0.003066
d
yr
n .9557226157315278 0.0028412 deg/d
Q 1.184040080874587 0.0023466 au
  Orbit Determination Parameters
   # obs. used (total)      25  
   data-arc span      1 day  
   first obs. used      2014-03-11  
   last obs. used      2014-03-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .35631  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:42:05  

Additional Information
 Earth MOID = .118745 au 
 Jupiter MOID = 4.08212 au 
 T_jup = 5.833 
[ 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 24.1   n/a MPO286775  

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