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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 ]

[ hide orbit diagram ]

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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5058806393427924 1.4885e-07  
a 1.628167812576457 8.2279e-08 au
q .804509238592923 2.068e-07 au
i 7.924784250623667 2.5853e-05 deg
node 224.0285204335084 0.00039059 deg
peri 166.3358579713134 0.00041471 deg
M 354.4421290887768 9.577e-05 deg
tp 2459212.215292302154
(2020-Dec-28.71529230)		 0.00020273 TDB
period 758.8346861850832
2.08		 5.7521e-05
1.575e-07		 d
yr
n .4744116295076611 3.5962e-08 deg/d
Q 2.45182638655999 1.239e-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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      1  
   norm. resid. RMS      .47542  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 17:21:07  

Additional Information
 Earth MOID = .0976586 au 
 Jupiter MOID = 3.00145 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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