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JPL Small-Body Database Browser
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(2015 FN34)
Classification: Apollo [NEO]          SPK-ID: 3713974
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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Orbit Diagram
[ switch to new HTML5 viewer ]

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 2457103.5 (2015-Mar-22.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4239434094408613 0.0016651  
a 1.574046324339403 0.0040902 au
q .9067397589811006 0.00027584 au
i 11.158166042001 0.031371 deg
node 179.7863299092492 6.1912e-05 deg
peri 53.49525175581681 0.016585 deg
M 339.1019788570053 0.095749 deg
tp 2457145.372351848905
(2015-May-02.87235185)
0.029796 TDB
period 721.3145475574757
1.97
2.8115
0.007697
d
yr
n .4990887834149976 0.0019454 deg/d
Q 2.241352889697705 0.0058242 au
  Orbit Determination Parameters
   # obs. used (total)      27  
   data-arc span      1 day  
   first obs. used      2015-03-21  
   last obs. used      2015-03-22  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .44475  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:58  

Additional Information
 Earth MOID = .0199325 au 
 Jupiter MOID = 2.78587 au 
 T_jup = 4.283 
[ show covariance matrix ]

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 26.7   n/a MPO332798  

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2015-Mar-25 05:18 < 00:01 Earth 0.0205593890331793 0.0203728110285717 0.0207459600139689 11.4900558297287 11.4787710435754 2457106.721012366 0.845937897453729 9284.38033488694 316.704500152227 0.342674290335527 219.105888653775 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 04:25:58 2018-Dec-11 16:36
2015-Aug-10 00:39 1_08:37 Earth 0.48891085701958 0.483936741536022 0.49390801868652 6.51746080468412 6.51662456242668 2457244.526802477 1957.13134970091 303478.094422277 67999.2375743943 -36.0761241784183 456.345268170436 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 04:25:58 2018-Dec-11 16:36
2017-Mar-12 03:03 7_11:34 Earth 0.18677199120256 0.0412136614554073 0.332399185516406 16.2730266480596 16.2721499622622 2457824.626994317 10774.1077056455 7262324.75800521 471.351011214244 -0.991191497400806 886.095305621846 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 04:25:58 2018-Dec-11 16:36
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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