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JPL Small-Body Database Browser
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(2007 FY20)
Classification: Apollo [NEO]          SPK-ID: 3372733
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 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3869999716580808 1.7439e-06  
a 1.45849053760067 1.1959e-07 au
q .894054740885632 2.4702e-06 au
i 5.372180426939197 4.4647e-05 deg
node 11.83966374830001 1.7592e-05 deg
peri 230.4162214938902 0.00053632 deg
M 283.6222431095623 0.00049016 deg
tp 2458736.995473514792
(2019-Sep-10.49547351)
0.00089275 TDB
period 643.3596961457401
1.76
7.9126e-05
2.166e-07
d
yr
n .5595625622131748 6.882e-08 deg/d
Q 2.022926334315708 1.6586e-07 au
  Orbit Determination Parameters
   # obs. used (total)      66  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      2531 days (6.93 yr)  
   first obs. used      2007-03-26  
   last obs. used      2014-02-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .44215  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:06:38  

Additional Information
 Earth MOID = .00153347 au 
 Jupiter MOID = 3.00958 au 
 T_jup = 4.540 
[ 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 25.0   n/a MPO289430  

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