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(2016 OZ2)
Classification: Apollo [NEO]          SPK-ID: 3674824
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 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5059870067684827 1.4912e-07  
a 1.628184952838877 8.2175e-08 au
q .8043445220864502 2.0733e-07 au
i 7.925752121468362 2.5884e-05 deg
node 224.0368620583821 0.00039216 deg
peri 166.3355995214582 0.00041628 deg
M 259.5650018004383 8.8975e-05 deg
tp 2459212.207677311281
(2020-Dec-28.70767731)
0.00020298 TDB
period 758.8466689731461
2.08
5.7449e-05
1.573e-07
d
yr
n .4744041381734517 3.5915e-08 deg/d
Q 2.452025383591304 1.2375e-07 au
  Orbit Determination Parameters
   # obs. used (total)      44  
   data-arc span      950 days (2.60 yr)  
   first obs. used      2014-06-24  
   last obs. used      2017-01-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .47367  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:24:48  

Additional Information
 Earth MOID = .0976062 au 
 Jupiter MOID = 3.00008 au 
 T_jup = 4.152 
[ 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 20.8   n/a E2016-RA8  

[ show close-approach data ]
Alternate Designations
 2016 OZ2 = 2014 MQ67 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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