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(2010 FD)
Classification: Amor [NEO]          SPK-ID: 3511916
Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Close-Approach Data ]

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Orbit Diagram
Note: Make sure you have Java enabled on your browser to see the applet. This applet is provided as a 3D orbit visualization tool. The applet was implemented using 2-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances. For accurate long-term ephemerides, please instead use our Horizons system.
Orbit Viewer

Additional Notes: the orbits shown in the applet are color coded. The planets are white lines, and the asteroid/comet is a blue line. The bright white line indicates the portion of the orbit that is above the ecliptic plane, and the darker portion is below the ecliptic plane. Likewise for the asteroid/comet orbit, the light blue indicates the portion above the ecliptic plane, and the dark blue the portion below the ecliptic plane.

Orbit Viewer applet originally written and kindly provided by Osamu Ajiki (AstroArts), and further modified by Ron Baalke (JPL).


Orbital Elements at Epoch 2456400.5 (2013-Apr-18.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6321895988149868 0.00089798  
a 2.873875060848684 0.0070762 AU
q 1.057041139086359 2.2036e-05 AU
i .3473738955642748 0.00037233 deg
node 22.32630319970087 0.0020652 deg
peri 162.7447636142943 0.0014911 deg
M 226.8169018528279 0.8407 deg
tp 2457058.834879058263
(2015-Feb-05.33487906)
6.5871 JED
period 1779.509260244725
4.87
6.5724
0.01799
d
yr
n .2023029652290157 0.00074718 deg/d
Q 4.69070898261101 0.01155 AU
  Orbit Determination Parameters
   # obs. used (total)      43  
   data-arc span      30 days  
   first obs. used      2010-03-16  
   last obs. used      2010-04-15  
   planetary ephem.      DE405  
   SB-pert. ephem.      SB405-CPV-2  
   condition code      7  
   fit RMS      .60408  
   data source      ORB  
   producer      Otto Matic  
   solution date      2011-Sep-14 20:51:16  

Additional Information
 Earth MOID = .0591279 AU 
 T_jup = 2.962 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 26.016 mag .31768 10 autocmod 2.5a

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