15P/Finlay (2014)

Japanese version
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 Updated on July 31, 2010

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* Profile

* Orbital Elements

Perturbed ephemeris below is based on elements from MPC 63377.

Epoch (TT/JD) T (TT/JD)         Peri.     Node      Incl.   
2457000.50000 2457018.4320591 347.55590  13.77655   6.79871 

    e             q             a      Epoch (TT)
0.7201878     0.9758961      3.48768  2014/12/09.00

* Finding Charts

* Magnitudes Graph

        m1 =  9.5 + 5 log d + 30.0 log r(t - 20)  [   , 20]  (             - 2015 Jan. 16)
        m1 =  9.4 + 5 log d + 25.0 log r(t - 20)  [ 20,145]  (2015 Jan. 16 - 2015 May  21)
        m1 = 13.2 + 5 log d + 10.0 log r          [145,   ]  (2015 May  21 -             )

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The orbital elements are calculated using the Minor Planet & Comet Ephemeris Service.
The charts are made with StellaNavigator Ver.8 (AstroArts).
The magnitudes graphs are made with Comet for Windows.

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