155P/Shoemaker 3 (2019)

Japanese version
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Updated on October 11, 2019

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* Profile

* Pictures

* Orbital Elements

Perturbed ephemeris below is based on elements from MPC 47729. 

 Epoch = 2458800.50000 TT   T = 2458802.69636 TT
 Peri. =   14.66594         a =     6.5903075 AU
 Node  =   97.19789 J2000.0 e =     0.7265915
 Incl. =    6.39595         q =     1.8018463 AU

* Finding Charts

* Magnitudes Graph

        m1 = 7.5 + 5 log d + 27 log r(t - 28)

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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.