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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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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer 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.


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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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