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(2015 FP124)
Classification: Apollo [NEO]          SPK-ID: 3714589
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 2457114.5 (2015-Apr-02.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4130352799754369 0.0010022  
a 1.708546758344721 0.0030225 au
q 1.002856669660684 6.1768e-05 au
i 27.37864043379605 0.033113 deg
node 9.409673792724748 0.0024528 deg
peri 219.1590166570161 0.024139 deg
M 346.3622433025153 0.04944 deg
tp 2457145.401471986934
(2015-May-02.90147199)
0.030025 TDB
period 815.7155287385326
2.23
2.1646
0.005926
d
yr
n .4413303257285341 0.0011711 deg/d
Q 2.414236847028758 0.0042709 au
  Orbit Determination Parameters
   # obs. used (total)      103  
   data-arc span      15 days  
   first obs. used      2015-03-27  
   last obs. used      2015-04-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .39206  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:40  

Additional Information
 Earth MOID = .0678957 au 
 Jupiter MOID = 2.70285 au 
 T_jup = 3.972 
[ 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 22.2   n/a MPO339527  

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