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(2014 FO38)
Classification: Aten [NEO]          SPK-ID: 3666685
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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4036948204576123 2.4866e-07  
a .7387893445664311 1.2642e-09 au
q .4405439127556886 1.8389e-07 au
i 9.694463287264291 2.8388e-05 deg
node 10.36869850184486 5.6269e-06 deg
peri 14.43665965034064 4.8979e-05 deg
M 297.7947554078688 0.00010278 deg
tp 2459436.577798992304
(2021-Aug-10.07779899)
6.6207e-05 TDB
period 231.9419806453811
0.64
5.9536e-07
1.63e-09
d
yr
n 1.552112295490002 3.984e-09 deg/d
Q 1.037034776377173 1.7746e-09 au
  Orbit Determination Parameters
   # obs. used (total)      85  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      2573 days (7.04 yr)  
   first obs. used      2014-03-28  
   last obs. used      2021-04-13  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .45711  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 09:12:57  

Additional Information
 Earth MOID = .0120332 au 
 Jupiter MOID = 4.41875 au 
 T_jup = 7.723 
[ 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 26.34   n/a E2021-GK1  

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