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(2014 EY24)
Classification: Apollo [NEO]          SPK-ID: 3663829
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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5987144106337982 6.6632e-09  
a 2.508975699444988 4.9006e-09 au
q 1.00681579225726 1.8031e-08 au
i 3.517488946672223 4.4893e-06 deg
node 6.137732275889398 1.7864e-05 deg
peri 160.0631919722065 2.4497e-05 deg
M 252.5712883787911 4.1437e-06 deg
tp 2459633.672598071156
(2022-Feb-23.17259807)
1.7833e-05 TDB
period 1451.587131152279
3.97
4.2529e-06
1.164e-08
d
yr
n .2480044030937569 7.2661e-10 deg/d
Q 4.011135606632716 7.8346e-09 au
  Orbit Determination Parameters
   # obs. used (total)      212  
   # delay obs. used      3  
   # Doppler obs. used      1  
   data-arc span      1444 days (3.95 yr)  
   first obs. used      2014-03-11  
   last obs. used      2018-02-22  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .33839  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 09:30:33  

Additional Information
 Earth MOID = .0199756 au 
 Jupiter MOID = .966063 au 
 T_jup = 3.184 
[ 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 MPO292237  

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