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JPL Small-Body Database Browser
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413209 (2003 FF35)
Classification: Main-belt Asteroid          SPK-ID: 2413209
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1876868329931626 5.7155e-08  
a 2.64607964313555 1.4604e-08 au
q 2.14944533506776 1.5128e-07 au
i 4.489582536463611 6.9893e-06 deg
node .1168605242162868 5.8104e-05 deg
peri 162.6275912483158 6.0705e-05 deg
M 11.46156617765826 1.4962e-05 deg
tp 2458950.445369483900
(2020-Apr-10.94536948)		 6.5227e-05 TDB
period 1572.181908343479
4.30		 1.3015e-05
3.563e-08		 d
yr
n .2289811363999933 1.8956e-09 deg/d
Q 3.142713951203339 1.7345e-08 au
   Orbit Determination Parameters
   # obs. used (total)      217  
   data-arc span      6160 days (16.87 yr)  
   first obs. used      2003-03-23  
   last obs. used      2020-02-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57683  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-26 06:58:58  

Additional Information
 Earth MOID = 1.15785 au 
 Jupiter MOID = 1.83557 au 
 T_jup = 3.363 
[ show covariance matrix ]

[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.8   n/a MPO419032  

413209 (2003 FF35)          Discovered 2003-Mar-23 by Spacewatch at Kitt Peak
Reference: Last Updated: 2014-11-10

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[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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