118P/Shoemaker-Levy 4 (2022)

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Updated on December 31, 2017

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 - )

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.