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(2018 OZ)
Classification: Apollo [NEO]          SPK-ID: 3825828
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 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2445743655790968 0.00047161  
a 1.032053839428321 0.0003146 au
q .7796399264066687 0.00024907 au
i 11.84457769709921 0.025243 deg
node 132.5484855021946 0.0022663 deg
peri 283.0417727499322 0.033181 deg
M 191.0604316516389 0.19772 deg
tp 2459180.213555743931
(2020-Nov-26.71355574)
0.2925 TDB
period 382.9587153579501
1.05
0.17511
0.0004794
d
yr
n .9400491112038261 0.00042984 deg/d
Q 1.284467752449974 0.00039155 au
  Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      15 days  
   first obs. used      2018-07-22  
   last obs. used      2018-08-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .29008  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Aug-07 07:00:35  

Additional Information
 Earth MOID = .00837131 au 
 Jupiter MOID = 4.01662 au 
 T_jup = 5.887 
[ 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 24.9   n/a E2018P08  

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