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(2016 EO56)
Classification: Aten [NEO]          SPK-ID: 3745901
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2457452.5 (2016-Mar-05.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6478204594189423 0.0018677  
a .9890209573470871 0.0042573 au
q .348312946383535 0.00034792 au
i 43.19803064876875 0.34794 deg
node 163.0951523037721 0.012862 deg
peri 222.6577137949659 0.14921 deg
M 66.95896948976142 0.57296 deg
tp 2457385.679006441101
(2015-Dec-29.17900644)
0.14033 TDB
period 359.2581825035694
0.98
2.3197
0.006351
d
yr
n 1.002064859013819 0.0064702 deg/d
Q 1.629728968310639 0.0070153 au
  Orbit Determination Parameters
   # obs. used (total)      24  
   data-arc span      8 days  
   first obs. used      2016-03-01  
   last obs. used      2016-03-09  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .36643  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:27:41  

Additional Information
 Earth MOID = .0643567 au 
 Jupiter MOID = 4.00631 au 
 T_jup = 5.745 
[ 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 MPO370802  

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