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JPL Small-Body Database Browser
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(2010 FX9)
Classification: Apollo [NEO]          SPK-ID: 3512704
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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3669295742320483 1.2939e-06  
a 1.131147056944802 2.8502e-08 au
q .7160957489462115 1.4814e-06 au
i 3.781603232012044 4.002e-05 deg
node 10.11411000048468 5.6228e-05 deg
peri 75.06136033246449 0.00014574 deg
M 191.4238055464558 2.7416e-05 deg
tp 2459602.264655061186
(2022-Jan-22.76465506)
3.8935e-05 TDB
period 439.4171790515805
1.20
1.6608e-05
4.547e-08
d
yr
n .8192670135860614 3.0965e-08 deg/d
Q 1.546198364943393 3.896e-08 au
  Orbit Determination Parameters
   # obs. used (total)      98  
   data-arc span      2204 days (6.03 yr)  
   first obs. used      2010-03-21  
   last obs. used      2016-04-02  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .35768  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 03:37:27  

Additional Information
 Earth MOID = .013917 au 
 Jupiter MOID = 3.6809 au 
 T_jup = 5.466 
[ 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 24.2   n/a MPO175362  
diameter diameter 0.030 km 0.002 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2014ApJ...784..110M)  
geometric albedo albedo 0.425   0.068 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2014ApJ...784..110M)  

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