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(2016 JX24)
Classification: Aten [NEO]          SPK-ID: 3753135
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2178085782881538 0.00021332  
a .8892195690355906 7.8894e-05 au
q .6955399189179438 0.0002514 au
i 7.194237041589702 0.0093259 deg
node 227.0120010249119 0.00022527 deg
peri 217.1483294282527 0.00055019 deg
M 70.28508027294718 0.21304 deg
tp 2458940.703937280844
(2020-Apr-01.20393728)
0.17329 TDB
period 306.27527912466
0.84
0.04076
0.0001116
d
yr
n 1.175413180681399 0.00015643 deg/d
Q 1.082899219153237 9.6078e-05 au
  Orbit Determination Parameters
   # obs. used (total)      60  
   data-arc span      18 days  
   first obs. used      2016-05-10  
   last obs. used      2016-05-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .28281  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:25:57  

Additional Information
 Earth MOID = .00998218 au 
 Jupiter MOID = 4.07931 au 
 T_jup = 6.652 
[ 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 25.4   n/a MPO382823  

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