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(2014 FN33)
Classification: Amor [NEO]          SPK-ID: 3666630
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 48 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4980224045509398 4.2678e-06  
a 2.211264932075916 2.0349e-05 au
q 1.110005453504298 7.8042e-07 au
i 6.085296970959655 3.7328e-05 deg
node 124.5702497204221 6.4025e-05 deg
peri 116.6497041217738 6.3128e-05 deg
M 300.1988382741182 0.0090827 deg
tp 2459200.010940032120
(2020-Dec-16.51094003)
0.033056 TDB
period 1201.045871663695
3.29
0.016579
4.539e-05
d
yr
n .2997387597705374 4.1375e-06 deg/d
Q 3.312524410647534 3.0483e-05 au
  Orbit Determination Parameters
   # obs. used (total)      216  
   data-arc span      145 days  
   first obs. used      2014-03-24  
   last obs. used      2014-08-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .37877  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:41:55  

Additional Information
 Earth MOID = .135975 au 
 Jupiter MOID = 1.74716 au 
 T_jup = 3.477 
[ 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 21.0   n/a MPO311396  
rotation period rot_per 6. h n/a LCDB (Rev. 2019-August); Warner et al., 2009 lower-limit; Incomplete or inconclusive result.
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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