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(2014 FS52)
Classification: Apollo [NEO]          SPK-ID: 3666886
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5861253260085896 1.9927e-05  
a 2.009165938783064 0.00010081 au
q .8315428979084865 1.8612e-06 au
i .8085456588248121 5.8474e-05 deg
node 128.1993709577166 0.0059372 deg
peri 133.633709603536 0.0065804 deg
M 41.45515114945091 0.057013 deg
tp 2458880.716185352283
(2020-Feb-01.21618535)
0.15572 TDB
period 1040.212665434927
2.85
0.07829
0.0002143
d
yr
n .3460830770114484 2.6047e-05 deg/d
Q 3.18678897965764 0.0001599 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.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .51136  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:41:49  

Additional Information
 Earth MOID = .00312794 au 
 Jupiter MOID = 1.91196 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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