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Updated on March 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. 2461800.50000 2461813.8908725 184.80377 66.57366 10.45600 e q a Epoch (TT) 0.4635046 1.7716322 3.30223 2028/01/30.00
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Finding Charts
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Magnitudes Graphm1 = 14.0 + 5 log d + 7.5 log r [ ,-635] ( - 2026 May 18) m1 = 7.5 + 5 log d + 18.0 log r(t + 15) [-635, 310] (2026 May 18 - 2028 Dec. 18) m1 = 11.5 + 5 log d + 10.0 log r [ 310, ] (2028 Dec. 18 - )
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The orbital elements are calculated using the Minor Planet & Comet Ephemeris Service.
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