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JPL Small-Body Database Browser
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(2019 BE5)
Classification: Aten [NEO]          SPK-ID: 3838078
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6591252009168106 2.2021e-07  
a .6101118603213679 4.3477e-08 au
q .2079717578053172 1.4873e-07 au
i 1.436252408904456 1.2587e-05 deg
node 309.0270530783652 3.2192e-05 deg
peri 9.755823661956544 3.0686e-05 deg
M 75.34709242275338 7.7993e-05 deg
tp 2458964.068535859758
(2020-Apr-24.56853586)
3.5223e-05 TDB
period 174.0654704616909
0.48
1.8606e-05
5.094e-08
d
yr
n 2.068187326556707 2.2107e-07 deg/d
Q 1.012251962837419 7.2134e-08 au
  Orbit Determination Parameters
   # obs. used (total)      82  
   data-arc span      363 days  
   first obs. used      2019-01-31  
   last obs. used      2020-01-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      2  
   norm. resid. RMS      .45254  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-01 05:46:11  

Additional Information
 Earth MOID = 1.04304E-5 au 
 Jupiter MOID = 4.30041 au 
 T_jup = 9.043 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458686.5 (2019-Jul-22.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6588769986625904 2.2087e-07  
q .2081771658938472 1.4945e-07 au
tp 2458615.797508188009
(2019-May-12.29750819)
3.2071e-05 TDB
node 309.1783951905617 3.1693e-05 deg
peri 9.585461649729012 3.0244e-05 deg
i 1.444118034870679 1.2639e-05 deg
  Orbit Determination Parameters
   # obs. used (total)      82  
   data-arc span      363 days  
   first obs. used      2019-01-31  
   last obs. used      2020-01-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      2  
   norm. resid. RMS      .45254  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-01 05:46:11  

Additional Information
 Jupiter MOID = 4.30041 au 
 T_jup = 9.043 
Orbit Covariance (6×6)
  e q tp node peri i
e 4.878517716578071E-14 -3.299758242163151E-14 4.779622834723839E-12 1.242655994368565E-12 2.12842282628562E-12 4.046098559341469E-13
q -3.299758242163151E-14 2.233536568065635E-14 -3.161622249812669E-12 -8.188199179959707E-13 -1.423798886076913E-12 -2.698214407256704E-13
tp 4.779622834723839E-12 -3.161622249812669E-12 1.028575551478037E-9 4.006880195386076E-10 2.67379919432497E-10 8.045173868231483E-11
node 1.242655994368565E-12 -8.188199179959707E-13 4.006880195386076E-10 1.004461283493865E-9 -7.38987833703109E-10 3.494719511123465E-10
peri 2.12842282628562E-12 -1.423798886076913E-12 2.67379919432497E-10 -7.38987833703109E-10 9.147077759350357E-10 -2.958174335030922E-10
i 4.046098559341469E-13 -2.698214407256704E-13 8.045173868231483E-11 3.494719511123465E-10 -2.958174335030922E-10 1.597432646776718E-10

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 25.1   .48425 MPO467428 autocmod 2.6q
rotation period rot_per 0.0033276 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Published Reference List:
[Ryan, W. (2019)http://infohost.nmt.edu/~bryan/research/work/mro_images/ztf02 rm/ztf02rm_190202_short.jpg]

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