129P/Shoemaker-Levy 3 (2022)

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Updated on May 24, 2022

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Orbital Elements Perturbed ephemeris below is based on elements from MPEC 2022-K19. Epoch (TT/JD) T (TT/JD) Peri. Node Incl. 2459920.50000 2459913.5412146 307.44461 184.86202 3.44235 e q a Epoch (TT) 0.0848379 3.9243700 4.28817 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 - )

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