145P/Shoemaker-Levy 5 (2017)

Japanese version
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Updated on August 11, 2016

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* Profile

* Orbital Elements

Perturbed ephemeris below is based on elements from MPC 56803.

Epoch (TT/JD) T (TT/JD)         Peri.     Node      Incl.   
2458000.50000 2457997.4293332  10.36776  26.81043  11.25980 

    e             q             a      Epoch (TT)
0.5407883     1.9041171      4.14649  2017/09/04.00

* Finding Charts

* Magnitudes Graph

        m1 = 10.5 + 5 log d + 15.0 log r(t - 70)

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The orbital elements are calculated using the Minor Planet & Comet Ephemeris Service.
The charts are made with StellaNavigator Ver.10 (AstroArts).
The magnitudes graphs are made with Comet for Windows.

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Copyright(C) Seiichi Yoshida (comet@aerith.net). All rights reserved.