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(2016 TA)
Classification: Apollo [NEO]          SPK-ID: 3760061
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2457663.5 (2016-Oct-02.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .8907558816723483 0.00046764  
a 2.38425884652356 0.0080305 au
q .2604662555533701 0.00023772 au
i 7.214829760596869 0.0085649 deg
node 6.63392257921504 0.0010952 deg
peri 127.4565801951398 0.0038447 deg
M 349.2933280991402 0.060191 deg
tp 2457703.492681492216
(2016-Nov-10.99268149)
0.022779 TDB
period 1344.709679208684
3.68
6.7938
0.0186
d
yr
n .2677157795219022 0.0013526 deg/d
Q 4.508051437493751 0.015184 au
  Orbit Determination Parameters
   # obs. used (total)      49  
   data-arc span      1 day  
   first obs. used      2016-10-01  
   last obs. used      2016-10-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .24539  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:23:30  

Additional Information
 Earth MOID = .00589623 au 
 Jupiter MOID = .698144 au 
 T_jup = 2.793 
[ 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 26.3   n/a E2016T21  

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