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(2014 JR24)
Classification: Apollo [NEO]          SPK-ID: 3670633
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456781.5 (2014-May-04.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1497826148643668 1.2766e-05  
q .9723084627026457 3.1026e-06 au
tp 2456826.098888873661
(2014-Jun-17.59888887)
0.00015277 TDB
node 225.1493493789915 1.0076e-05 deg
peri 45.69121789201112 0.00020493 deg
i 1.461232787646653 9.6335e-05 deg
  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
 Jupiter MOID = 3.88887 au 
 T_jup = 5.778 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.629706497921704E-10 -3.959070287276977E-11 -1.854771744438335E-9 1.111567788275273E-10 2.529522676171376E-9 1.228603959442325E-9
q -3.959070287276977E-11 9.626413956846727E-12 4.462288480646872E-10 -2.721348600183303E-11 -6.193002529867056E-10 -2.983599649027983E-10
tp -1.854771744438335E-9 4.462288480646872E-10 2.333801466786986E-8 -1.16414501808255E-9 -2.632792907118187E-8 -1.403426050302378E-8
node 1.111567788275273E-10 -2.721348600183303E-11 -1.16414501808255E-9 1.015162044112248E-10 1.816342693587253E-9 8.421541093064154E-10
peri 2.529522676171376E-9 -6.193002529867056E-10 -2.632792907118187E-8 1.816342693587253E-9 4.199817935665927E-8 1.900590774420657E-8
i 1.228603959442325E-9 -2.983599649027983E-10 -1.403426050302378E-8 8.421541093064154E-10 1.900590774420657E-8 9.280463932125677E-9

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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