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(2015 PM307)
Classification: Apollo [NEO, PHA]          SPK-ID: 3726510
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 2457249.5 (2015-Aug-15.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .8607199133727426 0.0023571  
a 2.184568019863367 0.032947 au
q .3042668230497059 0.00056047 au
i 8.037905444741723 0.044086 deg
node 142.1075266128104 0.0681 deg
peri 319.1646374742832 0.10128 deg
M 343.9641183736404 0.39394 deg
tp 2457302.033595447867
0.10211 TDB
period 1179.361060519718
n .30525003075933 0.0069055 deg/d
Q 4.064869216677027 0.061305 au
  Orbit Determination Parameters
   # obs. used (total)      20  
   data-arc span      11 days  
   first obs. used      2015-08-12  
   last obs. used      2015-08-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .55208  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:32:23  

Additional Information
 Earth MOID = .0446628 au 
 Jupiter MOID = 1.21644 au 
 T_jup = 3.035 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 5.555930048075456E-6 -1.321002338618786E-6 -.000240677889843125 .000160516900861205 -.0002387150327968207 .0001039142207721305
q -1.321002338618786E-6 3.141313649750436E-7 5.722539710853261E-5 -3.816438947109839E-5 5.675172905995708E-5 -2.470654621444545E-5
tp -.000240677889843125 5.722539710853261E-5 .01042596319937059 -.006953433078606261 .01034081267131587 -.004501460571589454
node .000160516900861205 -3.816438947109839E-5 -.006953433078606261 .004637563727498184 -.00689689182500472 .003002229729465085
peri -.0002387150327968207 5.675172905995708E-5 .01034081267131587 -.00689689182500472 .01025749718350937 -.004464860001426456
i .0001039142207721305 -2.470654621444545E-5 -.004501460571589454 .003002229729465085 -.004464860001426456 .001943560535643322

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 21.7   n/a MPO344285  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
FirstGov 2020-Aug-04 17:53 UT
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