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(2014 FS52)
Classification: Apollo [NEO]          SPK-ID: 3666886
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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5860421382483351 1.9798e-05  
a 2.009311856926266 9.9335e-05 au
q .8317704398854645 1.5402e-06 au
i .808559767449791 5.7658e-05 deg
node 128.1983796410197 0.0058191 deg
peri 133.6422927686346 0.0064676 deg
M 110.6486180831399 0.061542 deg
tp 2458880.748241996666
(2020-Feb-01.24824200)
0.15413 TDB
period 1040.32598757544
2.85
0.077146
0.0002112
d
yr
n .346045378371262 2.5661e-05 deg/d
Q 3.186853273967068 0.00015755 au
  Orbit Determination Parameters
   # obs. used (total)      59  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      15 days  
   first obs. used      2014-03-31  
   last obs. used      2014-04-15  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      5  
   norm. resid. RMS      .50898  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 09:42:07  

Additional Information
 Earth MOID = .00317144 au 
 Jupiter MOID = 1.91107 au 
 T_jup = 3.597 
[ 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 24.5   n/a MPO290435  

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