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(2011 OE26)
Classification: Apollo [NEO]          SPK-ID: 3574786
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7152702816132699 0.00053791  
a 3.00258774758948 0.0053045 au
q .8549259638025989 0.00010513 au
i 10.48722642950998 0.0072299 deg
node 315.2997474044562 0.00065454 deg
peri 272.0536829251239 0.0019007 deg
M 264.7320835691094 1.6622 deg
tp 2459503.405233619057
(2021-Oct-15.90523362)
10.107 TDB
period 1900.386729190148
5.20
5.036
0.01379
d
yr
n .1894351262668596 0.000502 deg/d
Q 5.15024953137636 0.0090987 au
  Orbit Determination Parameters
   # obs. used (total)      14  
   data-arc span      24 days  
   first obs. used      2011-07-26  
   last obs. used      2011-08-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .34207  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Oct-05 06:46:53  

Additional Information
 Earth MOID = .104253 au 
 Jupiter MOID = .96192 au 
 T_jup = 2.777 
[ 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 23.0   n/a MPO423762  

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