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JPL Small-Body Database Browser
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(2020 BM13)
Classification: Apollo [NEO]          SPK-ID: 3989298
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458878.5 (2020-Jan-30.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6240600932360835 0.0052545  
a 2.405091401759633 0.032637 au
q .9041698373362136 0.00037724 au
i 2.251849069080623 0.0094397 deg
node 142.4985928592617 0.073422 deg
peri 303.5727024774338 0.042439 deg
M 8.843871591421548 0.19999 deg
tp 2458845.031539733277
(2019-Dec-27.53153973)
0.077654 TDB
period 1362.372301708601
3.73
27.731
0.07592
d
yr
n .2642449494521511 0.0053787 deg/d
Q 3.906012966183051 0.053004 au
  Orbit Determination Parameters
   # obs. used (total)      14  
   data-arc span      1 day  
   first obs. used      2020-01-29  
   last obs. used      2020-01-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .28076  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jan-30 16:42:30  

Additional Information
 Earth MOID = .01207 au 
 Jupiter MOID = 1.36295 au 
 T_jup = 3.225 
[ 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 26.423   .3351 1 autocmod 2.8

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2020-Jan-22 23:57 01:21 Earth 0.0173356849765407 0.0171506913211674 0.0175206695257518 10.9924665490475 10.9784754230084 2458871.497930449 80.6624679742475 9203.43476342409 233.190921194001 -0.517734153063774 161.197047522335 T 1 CATAB v2.0f-lin.ifort 2020-Jan-30 16:42:32 2020-Jan-30 16:42
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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