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Updated on September 4, 2024 |
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Orbital ElementsPerturbed ephemeris below is based on elements from MPEC 2024-PC5. Epoch (TT/JD) T (TT/JD) Peri. Node Incl. 2460960.50000 2460976.5054847 357.91760 356.88123 13.03930 e q a Epoch (TT) 0.3180513 2.8074642 4.11683 2025/10/12.00
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Finding Charts
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Magnitudes Graphm1 = 11.5 + 5 log d + 10.0 log r [ ,-610] ( - 2024 Feb. 26) m1 = 3.0 + 5 log d + 24.0 log r(t + 20) [-610, 550] (2024 Feb. 26 - 2027 May 1) m1 = 11.5 + 5 log d + 10.0 log r [ 550, ] (2027 May 1 - )
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The orbital elements are calculated using the Minor Planet & Comet Ephemeris Service.
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