62P/Tsuchinshan 1 (2030)

Japanese version
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 Updated on May 30, 2025

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* Profile

* Orbital Elements

Perturbed ephemeris below is based on elements from MPEC 2025-DP4.

Epoch (TT/JD) T (TT/JD)         Peri.     Node      Incl.   
2462560.50000 2462566.3989890  47.41754  68.59669   4.73271 

    e             q             a      Epoch (TT)
0.6239716     1.2682946      3.37287  2030/02/28.00

* Finding Charts

* Magnitudes Graph

        m1 = 10.0 + 5 log d + 30.0 log r          [    ,-100]  (             - 2029 Nov. 25)
        m1 =  3.0 + 5 log d + 60   log r          [-100,   0]  (2029 Nov. 25 - 2030 Mar.  5)
        m1 =  6.2 + 5 log d + 28.0 log r(t - 10)  [   0,    ]  (2030 Mar.  5 -             )

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The orbital elements are calculated using the Minor Planet & Comet Ephemeris Service.
The charts are made with StellaNavigator Ver.11 (AstroArts).
The magnitudes graphs are made with Comet for Windows.

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