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(2011 OJ45)
Classification: Apollo [NEO]          SPK-ID: 3575154
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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Orbit Diagram
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Note: This Java-based orbit viewer will eventually be retired.

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 two-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.

Note: If the applet is not working, here are some notes that might help.
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2036079100587169 0.00029719  
a 1.01708305805678 1.896e-05 au
q .8099969022497104 0.00028717 au
i .7491018678626619 0.0016493 deg
node 288.930763614855 0.024684 deg
peri 135.5042944448041 0.054841 deg
M 128.7652931009337 0.28113 deg
tp 2458866.492416108742
(2020-Jan-17.99241611)
0.28883 TDB
period 374.6563149049598
1.03
0.010476
2.868e-05
d
yr
n .9608806409450813 2.6868e-05 deg/d
Q 1.22416921386385 2.282e-05 au
  Orbit Determination Parameters
   # obs. used (total)      21  
   data-arc span      17 days  
   first obs. used      2011-07-28  
   last obs. used      2011-08-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .38096  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:53:04  

Additional Information
 Earth MOID = .00758709 au 
 Jupiter MOID = 4.00208 au 
 T_jup = 5.982 
[ hide covariance matrix ]
Orbital Elements at Epoch 2455773.5 (2011-Jul-31.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2038041436007413 0.00030526  
q .8131002592087341 0.00022909 au
tp 2455870.228801956735
(2011-Nov-04.72880196)
0.031939 TDB
node 293.2839451215774 0.0062672 deg
peri 130.4537560395848 0.011937 deg
i .8298601535865058 0.0014566 deg
  Orbit Determination Parameters
   # obs. used (total)      21  
   data-arc span      17 days  
   first obs. used      2011-07-28  
   last obs. used      2011-08-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .38096  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:53:04  

Additional Information
 Jupiter MOID = 4.00208 au 
 T_jup = 5.982 
Orbit Covariance (6×6)
  e q tp node peri i
e 9.318660452287134E-8 -6.993307275755941E-8 -9.749698937807465E-6 1.910581320565718E-6 -3.64122200797229E-6 4.44633547029004E-7
q -6.993307275755941E-8 5.248255072687939E-8 7.316720047307726E-6 -1.43369756630326E-6 2.732366224543247E-6 -3.336734772616141E-7
tp -9.749698937807465E-6 7.316720047307726E-6 .00102007884350123 -.0001999156047636308 .0003810041231887926 -4.652123323909491E-5
node 1.910581320565718E-6 -1.43369756630326E-6 -.0001999156047636308 3.927779565299691E-5 -7.479556595521918E-5 9.121007702649214E-6
peri -3.64122200797229E-6 2.732366224543247E-6 .0003810041231887926 -7.479556595521918E-5 .0001424874339333306 -1.738075222217389E-5
i 4.44633547029004E-7 -3.336734772616141E-7 -4.652123323909491E-5 9.121007702649214E-6 -1.738075222217389E-5 2.121782732667251E-6

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 26.0   n/a MPO205911  

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