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(2017 FS102)
Classification: Apollo [NEO]          SPK-ID: 3773056
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2457843.5 (2017-Mar-31.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5112210714710248 0.00096616  
a 2.069324669741304 0.0041184 au
q 1.01144229485473 1.3689e-05 au
i 1.485707396722793 0.0020438 deg
node 25.59671301882639 0.0025775 deg
peri 184.3860768479644 0.003317 deg
M 354.1922694314707 0.016867 deg
tp 2457861.040636129368
(2017-Apr-17.54063613)
0.0014251 TDB
period 1087.279950759071
2.98
3.2459
0.008887
d
yr
n .3311014791992354 0.00098844 deg/d
Q 3.127207044627878 0.0062238 au
  Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      8 days  
   first obs. used      2017-03-28  
   last obs. used      2017-04-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .46167  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-05 06:18:29  

Additional Information
 Earth MOID = .00704972 au 
 Jupiter MOID = 1.83991 au 
 T_jup = 3.598 
[ 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 26.9   n/a MPO405728  

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