129P/Shoemaker-Levy 3 (2022)

Japanese version
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Updated on October 22, 2018

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* Profile

* Pictures

* Orbital Elements

Perturbed ephemeris below is based on elements from MPC 100284.

Epoch (TT/JD) T (TT/JD)         Peri.     Node      Incl.   
2459920.50000 2459913.5260876 307.44514 184.86265   3.44223 

    e             q             a      Epoch (TT)
0.0848237     3.9243665      4.28810  2022/12/07.00

* Magnitudes Graph

        m1 = -1768.5 + 5 log d + 3000   log r(t + 1640)  [-1630,-1505]  (2018 June 14 - 2018 Oct. 17)
        m1 =     7.7 + 5 log d +   15.0 log r            [-1505,     ]  (2018 Oct. 17 -             )

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The orbital elements are calculated using the Minor Planet & Comet Ephemeris Service.
The magnitudes graphs are made with Comet for Windows.

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