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(2014 FO38)
Classification: Aten [NEO]          SPK-ID: 3666685
[ 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4033775788198289 1.3764e-06  
a .738976160485178 5.1212e-07 au
q .4408897460630936 1.3059e-06 au
i 9.711647408835779 3.3864e-05 deg
node 10.41540396930367 6.6607e-06 deg
peri 14.4616902717373 9.705e-05 deg
M 43.20828427690701 0.0034919 deg
tp 2458972.651065097612
(2020-May-03.15106510)		 0.0022217 TDB
period 232.0299621389509
0.64		 0.0002412
6.604e-07		 d
yr
n 1.551523763057869 1.6128e-06 deg/d
Q 1.037062574907262 7.187e-07 au
   Orbit Determination Parameters
   # obs. used (total)      79  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      7 days  
   first obs. used      2014-03-28  
   last obs. used      2014-04-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .45451  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:41:52  

Additional Information
 Earth MOID = .0114902 au 
 Jupiter MOID = 4.41638 au 
 T_jup = 7.721 
[ 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 26.3   n/a MPO290420  

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