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 54480U 22151HG 24357.57409390 .00000905 00000-0 29074-3 0 9999
2 54480 98.6692 19.1655 0130437 182.6582 177.3926 14.37159298110499
| Epoch (UTC): | 22 December 2024 13:46:41 |
| Eccentricity: | 0.0130437 |
| inclination: | 98.6692° |
| perigee height: | 674 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 19.1655° |
| argument of perigee: | 182.6582° |
| revolutions per day: | 14.37159298 |
| mean anomaly at epoch: | 177.3926° |
| orbit number at epoch: | 11049 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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