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Updated on January 4, 2023 |
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Orbital ElementsPerturbed ephemeris below is based on elements from MPEC 2022-X67. Epoch (TT/JD) T (TT/JD) Peri. Node Incl. 2461640.50000 2461643.4788975 174.56311 92.55188 21.82813 e q a Epoch (TT) 0.6597734 1.1330860 3.33039 2027/08/23.00
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Finding Charts
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Magnitudes GraphH = 14.3 G = 0.15 [ ,-165] ( - 2027 Mar. 13) m1 = 11.7 + 5 log d + 12.5 log r(t - 50) [-165, 50] (2027 Mar. 13 - 2027 Oct. 14) m1 = 11.5 + 5 log d + 15.0 log r(t - 50) [ 50, 385] (2027 Oct. 14 - 2028 Sept.13) H = 15.8 G = 0.15 [ 385, ] (2028 Sept.13 - )
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The orbital elements are calculated using the Minor Planet & Comet Ephemeris Service.
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