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JPL Small-Body Database Browser
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(2018 FK5)
Classification: Apollo [NEO]          SPK-ID: 3802103
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.


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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2966687421609577 0.00016914  
a 1.094706525655439 9.1216e-05 au
q .7699413176538477 0.00012144 au
i 12.2210190319873 0.006337 deg
node 9.564520314427021 6.9571e-05 deg
peri 269.9346308333922 0.0054183 deg
M 281.1659805751638 0.028243 deg
tp 2458692.112799939604
(2019-Jul-27.61279994)
0.044272 TDB
period 418.3550226016661
1.15
0.052289
0.0001432
d
yr
n .8605131540222275 0.00010755 deg/d
Q 1.41947173365703 0.00011828 au
  Orbit Determination Parameters
   # obs. used (total)      33  
   data-arc span      1 day  
   first obs. used      2018-03-28  
   last obs. used      2018-03-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .35961  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Mar-29 17:12:02  

Additional Information
 Earth MOID = .000304801 au 
 Jupiter MOID = 3.73851 au 
 T_jup = 5.609 
[ 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 28.3   n/a E2018G02  

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