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(2019 BZ)
Classification: Apollo [NEO]          SPK-ID: 3837949
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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2716542772240144 0.0001176  
a 1.08712742349451 8.5156e-05 au
q .7918046090147036 6.5823e-05 au
i 6.737028636252802 0.0029703 deg
node 305.108375659109 0.00013433 deg
peri 92.20155287773954 9.0716e-05 deg
M 108.5871345917753 0.10376 deg
tp 2459271.619400180962
(2021-Feb-26.11940018)
0.10466 TDB
period 414.0178862244225
1.13
0.048646
0.0001332
d
yr
n .8695276508050632 0.00010217 deg/d
Q 1.382450237974316 0.00010829 au
  Orbit Determination Parameters
   # obs. used (total)      38  
   data-arc span      12 days  
   first obs. used      2019-01-24  
   last obs. used      2019-02-05  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .41983  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 21:03:29  

Additional Information
 Earth MOID = .000749287 au 
 Jupiter MOID = 4.02602 au 
 T_jup = 5.660 
[ 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 27.6   .34152 MPO467412 autocmod 2.6q

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