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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1183362477017753 1.5912e-05  
a 1.06640886553153 2.1362e-05 au
q .9402140418686213 1.8823e-06 au
i .9298680982409478 0.00040708 deg
node 48.88859643949959 0.001355 deg
peri 246.4304533273203 0.0071225 deg
M 126.3907578414766 0.05296 deg
tp 2458859.279786299804
(2020-Jan-10.77978630)		 0.054931 TDB
period 402.2388804396182
1.10		 0.012086
3.309e-05		 d
yr
n .8949905578658777 2.6892e-05 deg/d
Q 1.192603689194438 2.389e-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 = .00075253 au 
 Jupiter MOID = 3.88994 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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