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(2020 FF1)
Classification: Apollo [NEO]          SPK-ID: 54016222
[ 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 2458926.5 (2020-Mar-18.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4951741941930148 0.001172  
a 1.619296815337329 0.0031548 au
q .8174628196433521 0.00030525 au
i 1.997026978645407 0.0039641 deg
node 176.5776547049011 0.00027159 deg
peri 69.07954496329235 0.0048074 deg
M 336.367865394976 0.082176 deg
tp 2458975.907009796874
(2020-May-06.40700980)		 0.027415 TDB
period 752.6414276217505
2.06		 2.1995
0.006022		 d
yr
n .4783154192529016 0.0013978 deg/d
Q 2.421130811031306 0.004717 au
   Orbit Determination Parameters
   # obs. used (total)      20  
   data-arc span      7 days  
   first obs. used      2020-03-16  
   last obs. used      2020-03-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .3  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-04 06:25:58  

Additional Information
 Earth MOID = .00376027 au 
 Jupiter MOID = 2.61651 au 
 T_jup = 4.182 
[ 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 27.9   .67518 E2020G29 autocmod 2.8

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