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(2012 UU158)
Classification: Apollo [NEO]          SPK-ID: 3614981
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 2456226.5 (2012-Oct-26.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3740076406630594 0.002162  
a 1.100250639175492 0.0017443 AU
q .6887484934794433 0.0012868 AU
i 5.98537406527766 0.035015 deg
node 26.81681230711683 0.0033788 deg
peri 261.8296489489414 0.0015984 deg
M 60.69954443848415 0.26178 deg
tp 2456155.424683543055
(2012-Aug-15.92468354)
0.13751 JED
period 421.53716574317
1.15
1.0024
0.002744
d
yr
n .8540172237608517 0.0020308 deg/d
Q 1.511752784871542 0.0023966 AU
  Orbit Determination Parameters
   # obs. used (total)      11  
   data-arc span      14 days  
   first obs. used      2012-10-23  
   last obs. used      2012-11-06  
   planetary ephem.      DE405  
   SB-pert. ephem.      SB405-CPV-2  
   condition code      8  
   fit RMS      .82154  
   data source      ORB  
   producer      Otto Matic  
   solution date      2013-Jan-02 15:04:21  

Additional Information
 Earth MOID = .000907934 AU 
 T_jup = 5.578 
[ 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 26.896 mag .55951 4 autocmod 2.5b

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