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(2016 FL13)
Classification: Apollo [NEO]          SPK-ID: 3748478
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 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5760580616483248 0.0005035  
a 2.196599265622968 0.0024874 au
q .9312305504500674 5.1479e-05 au
i 8.443641485869685 0.0054768 deg
node 197.045420574286 0.00072825 deg
peri 47.76983205445607 0.0020047 deg
M 147.35758799858 0.86446 deg
tp 2458713.762640881897
(2019-Aug-18.26264088)
2.0286 TDB
period 1189.117246437324
3.26
2.0198
0.00553
d
yr
n .3027455880221943 0.00051424 deg/d
Q 3.461967980795869 0.0039203 au
  Orbit Determination Parameters
   # obs. used (total)      68  
   data-arc span      19 days  
   first obs. used      2016-03-28  
   last obs. used      2016-04-16  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .43139  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 16:46:54  

Additional Information
 Earth MOID = .0243009 au 
 Jupiter MOID = 1.61907 au 
 T_jup = 3.420 
[ 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 E2016G28  

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