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 54416U 22151EQ 24262.91273493 .00001306 00000-0 11079-2 0 9995
2 54416 98.8494 234.2082 0178714 61.5407 300.3623 13.82035346 93224
| Epoch (UTC): | 18 September 2024 21:54:20 |
| Eccentricity: | 0.0178714 |
| inclination: | 98.8494° |
| perigee height: | 825 km |
| apogee height: | 1088 km |
| right ascension of ascending node: | 234.2082° |
| argument of perigee: | 61.5407° |
| revolutions per day: | 13.82035346 |
| mean anomaly at epoch: | 300.3623° |
| orbit number at epoch: | 9322 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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