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(2017 TE5)
Classification: Apollo [NEO]          SPK-ID: 3785788
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .49381220602894 0.00015078  
a 1.815853634045524 0.00052195 au
q .9191629451918364 9.6008e-06 au
i 10.09074203459895 0.0023963 deg
node 23.17638852556715 0.00022127 deg
peri 41.79467294664657 0.00058375 deg
M 12.25432102968267 0.15995 deg
tp 2458970.076691673179
(2020-Apr-30.57669167)
0.38398 TDB
period 893.7574730681926
2.45
0.38535
0.001055
d
yr
n .4027938348466626 0.00017367 deg/d
Q 2.712544322899213 0.00077969 au
  Orbit Determination Parameters
   # obs. used (total)      83  
   data-arc span      3 days  
   first obs. used      2017-10-14  
   last obs. used      2017-10-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .48412  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Oct-19 06:18:51  

Additional Information
 Earth MOID = .00462911 au 
 Jupiter MOID = 2.68343 au 
 T_jup = 3.877 
[ 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 26.0   n/a MPO421501  

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