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(2013 FG)
Classification: Apollo [NEO]          SPK-ID: 3632679
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 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3944688798708648 0.00068335  
a 1.495842612187458 0.0014765 au
q .9057792524947628 0.00012811 au
i 3.024245147438165 0.0035025 deg
node 14.10636383559188 0.0039752 deg
peri 216.8098361945312 0.0010357 deg
M 313.9463983969346 2.0505 deg
tp 2459085.984697073897
(2020-Aug-24.48469707)
3.9327 TDB
period 668.2320139008312
1.83
0.98939
0.002709
d
yr
n .5387350388953763 0.00079766 deg/d
Q 2.085905971880152 0.0020589 au
  Orbit Determination Parameters
   # obs. used (total)      31  
   data-arc span      6 days  
   first obs. used      2013-03-17  
   last obs. used      2013-03-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .47384  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:46:23  

Additional Information
 Earth MOID = .0095094 au 
 Jupiter MOID = 2.91332 au 
 T_jup = 4.463 
[ 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 25.6   n/a MPO265052  

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