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JPL Small-Body Database Browser
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(2017 FU64)
Classification: Apollo [NEO]          SPK-ID: 3772392
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 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7076834722769222 1.3417e-06  
a 2.450335211769863 1.0251e-05 au
q .7162734808621589 3.6363e-07 au
i 6.91029469658264 2.9036e-05 deg
node 21.23256113152697 4.9181e-05 deg
peri 247.0734656301729 5.1197e-05 deg
M 181.7427231567765 0.0011297 deg
tp 2459294.215575097627
(2021-Mar-20.71557510)
0.0087496 TDB
period 1400.99529992702
3.84
0.0087913
2.407e-05
d
yr
n .2569601768248279 1.6124e-06 deg/d
Q 4.184396942677568 1.7505e-05 au
  Orbit Determination Parameters
   # obs. used (total)      194  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      15 days  
   first obs. used      2017-03-21  
   last obs. used      2017-04-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      2  
   norm. resid. RMS      .25662  
   source      ORB  
   producer      OSOD/JPL  
   solution date      2017-Jul-19 16:06:48  

Additional Information
 Earth MOID = .00946019 au 
 Jupiter MOID = 1.08378 au 
 T_jup = 3.086 
[ 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 23.8   n/a MPO411586  

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