View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 40911U 15049N 24261.16552073 .00273454 00000-0 27158-2 0 9998
2 40911 97.4609 284.6593 0001217 335.8672 24.2530 15.64885640498862
| Epoch (UTC): | 17 September 2024 03:58:20 |
| Eccentricity: | 0.0001217 |
| inclination: | 97.4609° |
| perigee height: | 373 km |
| apogee height: | 374 km |
| right ascension of ascending node: | 284.6593° |
| argument of perigee: | 335.8672° |
| revolutions per day: | 15.64885640 |
| mean anomaly at epoch: | 24.2530° |
| orbit number at epoch: | 49886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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