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(2014 JR24)
Classification: Apollo [NEO]          SPK-ID: 3670633
[ 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 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1183408295708416 1.5881e-05  
a 1.066410130778927 2.1379e-05 au
q .9402102712397992 1.9297e-06 au
i .9298600565946662 0.00040714 deg
node 48.88787414990826 0.001357 deg
peri 246.455539979492 0.0071028 deg
M 305.3595005488161 0.058371 deg
tp 2459261.551590113244
(2021-Feb-16.05159011)		 0.067055 TDB
period 402.2395962980438
1.10		 0.012096
3.312e-05		 d
yr
n .8949889650676115 2.6913e-05 deg/d
Q 1.192609990318055 2.3908e-05 au
   Orbit Determination Parameters
   # obs. used (total)      56  
   data-arc span      7 days  
   first obs. used      2014-04-30  
   last obs. used      2014-05-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .31286  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:40:37  

Additional Information
 Earth MOID = .000879586 au 
 Jupiter MOID = 3.88887 au 
 T_jup = 5.778 
[ 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 29.3   n/a MPO293438  

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