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(2014 BA3)
Classification: Aten [NEO]          SPK-ID: 3656792
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 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07474065392966599 3.1727e-05  
a .9395075329092317 2.017e-05 au
q .8692881255277486 4.8465e-05 au
i 2.258661824303965 0.00083368 deg
node 299.9068126511178 0.00094383 deg
peri 332.6506669409495 0.0029847 deg
M 205.5026140527256 0.079166 deg
tp 2459143.247155102207
(2020-Oct-20.74715510)
0.077742 TDB
period 332.6203580838065
0.91
0.010711
2.933e-05
d
yr
n 1.082314991403187 3.4854e-05 deg/d
Q 1.009726940290715 2.1678e-05 au
  Orbit Determination Parameters
   # obs. used (total)      70  
   data-arc span      8 days  
   first obs. used      2014-01-21  
   last obs. used      2014-01-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .63538  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:42:49  

Additional Information
 Earth MOID = .0101588 au 
 Jupiter MOID = 3.99788 au 
 T_jup = 6.385 
[ 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 28.2   n/a MPO284115  

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