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JPL Small-Body Database Browser
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(2020 FG)
Classification: Apollo [NEO]          SPK-ID: 54016200
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6494094127868265 0.00050537  
a 2.373132889921703 0.0031892 au
q .8319980534125454 8.1594e-05 au
i 1.82457803499955 0.00080579 deg
node 182.9374262184474 0.0021743 deg
peri 50.02328291733294 0.0027785 deg
M 9.763036607802547 0.017538 deg
tp 2458964.287047796423
(2020-Apr-24.78704780)
0.0079617 TDB
period 1335.308195287221
3.66
2.6917
0.007369
d
yr
n .2696006819029257 0.00054346 deg/d
Q 3.914267726430861 0.0052602 au
  Orbit Determination Parameters
   # obs. used (total)      34  
   data-arc span      1 day  
   first obs. used      2020-03-16  
   last obs. used      2020-03-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .34256  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Mar-17 07:49:12  

Additional Information
 Earth MOID = .00241336 au 
 Jupiter MOID = 1.09359 au 
 T_jup = 3.219 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458925.5 (2020-Mar-17.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6532813802022815 0.00050078  
q .8334869988968171 8.3909e-05 au
tp 2458964.048433884234
(2020-Apr-24.54843388)
0.0073974 TDB
node 183.2242948403056 0.0019611 deg
peri 49.37119711041939 0.0028616 deg
i 1.715792474233194 0.00095012 deg
  Orbit Determination Parameters
   # obs. used (total)      34  
   data-arc span      1 day  
   first obs. used      2020-03-16  
   last obs. used      2020-03-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .34256  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Mar-17 07:49:12  

Additional Information
 Jupiter MOID = 1.09359 au 
 T_jup = 3.219 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.507838872574494E-7 -4.186323715143196E-8 -3.696619055034238E-6 5.015391091384892E-7 3.496499141211281E-7 4.487709899062828E-7
q -4.186323715143196E-8 7.040708777424063E-9 6.135885608541943E-7 -7.202291748984112E-8 -7.819452749780121E-8 -7.707645369668141E-8
tp -3.696619055034238E-6 6.135885608541943E-7 5.472175521581273E-5 -8.15837998023021E-6 -3.847343165516079E-6 -6.473205267251697E-6
node 5.015391091384892E-7 -7.202291748984112E-8 -8.15837998023021E-6 3.846098836502851E-6 -3.943065895666176E-6 3.666182488903862E-7
peri 3.496499141211281E-7 -7.819452749780121E-8 -3.847343165516079E-6 -3.943065895666176E-6 8.189026059560325E-6 1.489516267463128E-6
i 4.487709899062828E-7 -7.707645369668141E-8 -6.473205267251697E-6 3.666182488903862E-7 1.489516267463128E-6 9.027251503740109E-7

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 27.894   .31112 1 autocmod 2.8

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