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(2017 TE5)
Classification: Apollo [NEO]          SPK-ID: 3785788
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4938366360759588 0.00015088  
a 1.815750065625998 0.00052288 au
q .9190661612625539 9.3154e-06 au
i 10.09131803418346 0.002395 deg
node 23.17437599153821 0.00022676 deg
peri 41.78684500386505 0.00054975 deg
M 92.81833518859496 0.19479 deg
tp 2458970.083379040665
(2020-Apr-30.58337904)
0.38402 TDB
period 893.6810100807852
2.45
0.38603
0.001057
d
yr
n .4028282977249986 0.000174 deg/d
Q 2.712433969989442 0.0007811 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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .48362  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 19:53:21  

Additional Information
 Earth MOID = .0038009 au 
 Jupiter MOID = 2.68439 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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