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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.


Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7076684563686545 1.6074e-06  
a 2.449289887351005 1.2185e-05 au
q .7160046935699634 4.3867e-07 au
i 6.910244055587281 3.146e-05 deg
node 21.183096399 5.4142e-05 deg
peri 247.1453853936583 5.6827e-05 deg
M 26.26779846919902 0.0028727 deg
tp 2459294.340234862228
(2021-Mar-20.84023486)
0.01041 TDB
period 1400.098888862817
3.83
0.010448
2.861e-05
d
yr
n .2571246951652092 1.9187e-06 deg/d
Q 4.182575081132045 2.0807e-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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      3  
   norm. resid. RMS      .22542  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 18:51:26  

Additional Information
 Earth MOID = .00928599 au 
 Jupiter MOID = 1.08512 au 
 T_jup = 3.087 
[ 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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