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JPL Small-Body Database Browser
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(2016 OZ2 = 2014 MQ67)
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5061456295484656 1.4922e-07  
a 1.628022259035982 8.2372e-08 au
q .8040059078172995 2.0743e-07 au
i 7.927040782299003 2.5884e-05 deg
node 224.0381741574475 0.00039209 deg
peri 166.3552614130653 0.0004162 deg
M 69.73426964760853 7.5268e-05 deg
tp 2458453.528647584148
(2018-Dec-01.02864758)		 0.00014817 TDB
period 758.7329319870665
2.08		 5.7584e-05
1.577e-07		 d
yr
n .4744752531792525 3.601e-08 deg/d
Q 2.452038610254664 1.2406e-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 = .0977278 au 
 Jupiter MOID = 2.99746 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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