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(2016 TT100)
Classification: Centaur          SPK-ID: 3841526
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 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5874357644732364 4.0138e-06  
a 8.902685211978438 9.1132e-05 au
q 3.672929518615307 2.5094e-06 au
i 9.709753058333487 1.7961e-05 deg
node 55.2588547494741 0.00013948 deg
peri 45.00154172136157 0.00018719 deg
M 35.56220499051385 0.00054504 deg
tp 2458042.057345242254
(2017-Oct-15.55734524)
0.00078873 TDB
period 9702.417378360738
26.56
0.14898
0.0004079
d
yr
n .03710415517713209 5.6972e-07 deg/d
Q 14.13244090534157 0.00014467 au
  Orbit Determination Parameters
   # obs. used (total)      54  
   data-arc span      1677 days (4.59 yr)  
   first obs. used      2014-09-22  
   last obs. used      2019-04-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .54681  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Apr-29 04:03:16  

Additional Information
 Earth MOID = 2.69924 au 
 Jupiter MOID = .26765 au 
 T_jup = 2.671 
[ 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 15.0   .42666 MPO466846 autocmod 2.6q

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