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 54472U 22151GY 24357.99759302 .00000340 00000-0 18223-3 0 9994
2 54472 98.8165 10.4238 0004814 145.5336 214.6153 14.19635111109254
| Epoch (UTC): | 22 December 2024 23:56:32 |
| Eccentricity: | 0.0004814 |
| inclination: | 98.8165° |
| perigee height: | 823 km |
| apogee height: | 830 km |
| right ascension of ascending node: | 10.4238° |
| argument of perigee: | 145.5336° |
| revolutions per day: | 14.19635111 |
| mean anomaly at epoch: | 214.6153° |
| orbit number at epoch: | 10925 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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