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(2019 BE3)
Classification: Apollo [NEO]          SPK-ID: 3838031
[ 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .594258879373016 0.00012993  
a 1.231584238445039 0.00021445 au
q .4997043690532206 7.3007e-05 au
i 8.507290968184146 0.0023908 deg
node 130.1077544649762 0.00050894 deg
peri 111.0052039546505 0.0010851 deg
M 309.1646270638675 0.07592 deg
tp 2459070.994968927453
(2020-Aug-09.49496893)		 0.12369 TDB
period 499.2230281415929
1.37		 0.13039
0.000357		 d
yr
n .7211205807955927 0.00018835 deg/d
Q 1.963464107836857 0.0003419 au
   Orbit Determination Parameters
   # obs. used (total)      22  
   data-arc span      29 days  
   first obs. used      2019-01-04  
   last obs. used      2019-02-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .41255  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Feb-07 07:05:22  

Additional Information
 Earth MOID = .00551246 au 
 Jupiter MOID = 3.08579 au 
 T_jup = 4.999 
[ 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 24.4   .32771 MPO467421 autocmod 2.6q

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