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(2010 FM)
Classification: Aten [NEO]          SPK-ID: 3512277
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 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2700830813915582 0.00034865  
a .8176590073983797 0.00017413 AU
q .5968231431526624 0.00041218 AU
i 7.741468415804787 0.013754 deg
node 175.3841766664758 0.00036782 deg
peri 202.3184124260771 0.0035529 deg
M 206.8727727595387 0.47535 deg
tp 2456515.370016297535
(2013-Aug-10.87001630)
0.39328 JED
period 270.0578245446455
0.74
0.086267
0.0002362
d
yr
n 1.333047841168866 0.00042583 deg/d
Q 1.038494871644097 0.00022116 AU
  Orbit Determination Parameters
   # obs. used (total)      32  
   data-arc span      6 days  
   first obs. used      2010-03-17  
   last obs. used      2010-03-23  
   planetary ephem.      DE405  
   SB-pert. ephem.      SB405-CPV-2  
   condition code      7  
   fit RMS      .7154  
   data source      ORB  
   producer      Otto Matic  
   solution date      2012-Jun-23 00:51:19  

Additional Information
 Earth MOID = .0110979 AU 
 T_jup = 7.120 
[ 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 27.097 mag .37824 7 autocmod 2.5b

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