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JPL Small-Body Database Browser
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(2017 FO)
Classification: Apollo [NEO]          SPK-ID: 3771584
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 2457830.5 (2017-Mar-18.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3227164249596033 0.0017718  
a 1.405113866767796 0.0034592 au
q .9516605430233283 0.00014701 au
i 13.86166189708099 0.055325 deg
node 176.0690192659517 0.0028223 deg
peri 47.73337227184079 0.012137 deg
M 335.8605982093341 0.112 deg
tp 2457871.293381712194
(2017-Apr-27.79338171)
0.038639 TDB
period 608.3670814936437
1.67
2.2465
0.006151
d
yr
n .5917479938528878 0.0021852 deg/d
Q 1.858567190512263 0.0045755 au
  Orbit Determination Parameters
   # obs. used (total)      26  
   data-arc span      2 days  
   first obs. used      2017-03-17  
   last obs. used      2017-03-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .66367  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:19:29  

Additional Information
 Earth MOID = .0298099 au 
 Jupiter MOID = 3.14613 au 
 T_jup = 4.658 
[ 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 26.4   n/a E2017F30  

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