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JPL Small-Body Database Browser
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(2015 FP)
Classification: Apollo [NEO]          SPK-ID: 3713319
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3476645379387672 0.00049147  
a 1.548640056760937 0.0011858 au
q 1.01023282699368 1.2452e-05 au
i 9.698986208330618 0.010228 deg
node 3.740645173670281 4.5322e-05 deg
peri 199.4436088964571 0.0028575 deg
M 35.07694337098624 0.86859 deg
tp 2458531.912748394462
(2019-Feb-17.41274839)
1.6196 TDB
period 703.9213855337591
1.93
0.80849
0.002214
d
yr
n .5114207458365887 0.00058739 deg/d
Q 2.087047286528195 0.001598 au
  Orbit Determination Parameters
   # obs. used (total)      52  
   data-arc span      8 days  
   first obs. used      2015-03-17  
   last obs. used      2015-03-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .53678  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:35:04  

Additional Information
 Earth MOID = .0247408 au 
 Jupiter MOID = 2.88078 au 
 T_jup = 4.368 
[ 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 25.2   n/a MPO332795  
rotation period rot_per 0.1872 h n/a LCDB (Rev. 2019-January); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Thirouin, A.; Moskovitz, N.; Binzel, R.P.; Christensen, E.; et al. (2016) Astron. J. 152, A163.]

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