Japanese version Home page |
Updated on March 4, 2023 |
Profile |
Orbital ElementsPerturbed ephemeris below is based on elements from MPEC 2022-ED3. Epoch (TT/JD) T (TT/JD) Peri. Node Incl. 2461800.50000 2461811.3463707 347.84070 13.72127 6.78310 e q a Epoch (TT) 0.7158419 0.9985749 3.51415 2028/01/30.00
|
Finding Charts
|
Magnitudes Graphm1 = 10.0 + 5 log d + 30.0 log r(t - 10) [ , 10] ( - 2028 Feb. 19) m1 = 10.0 + 5 log d + 25.0 log r(t - 10) [ 10,113] (2028 Feb. 19 - 2028 June 1) m1 = 13.2 + 5 log d + 10.0 log r [113, ] (2028 June 1 - )
|
The orbital elements are calculated using the Minor Planet & Comet Ephemeris Service.
|