118P/Shoemaker-Levy 4 (2022)

Japanese version
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Updated on December 31, 2017

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* Profile

* Orbital Elements

Perturbed ephemeris below is based on elements from MPC 95735.

Epoch (TT/JD) T (TT/JD)         Peri.     Node      Incl.   
2459920.50000 2459907.8076924 314.83383 142.09494  10.09197 

    e             q             a      Epoch (TT)
0.4534051     1.8290091      3.34619  2022/12/07.00

* Finding Charts

* Magnitudes Graph

        H = 14.5  G = 0.15                [    ,-425]  (             - 2021 Sept.25)
        m1 =  8.2 + 5 log d + 18.0 log r  [-425,-100]  (2021 Sept.25 - 2022 Aug. 16)
        m1 = -4.5 + 5 log d + 60.0 log r  [-100, 100]  (2022 Aug. 16 - 2023 Mar.  4)
        m1 =  8.2 + 5 log d + 18.0 log r  [ 100, 435]  (2023 Mar.  4 - 2024 Feb.  2)
        H = 14.5  G = 0.15                [ 435,    ]  (2024 Feb.  2 -             )

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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.