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 54579U 22151MF 23333.55273847 .00017809 00000-0 51039-2 0 9991
2 54579 98.6290 344.6947 0101264 249.3345 109.6964 14.42027888 54252
| Epoch (UTC): | 29 November 2023 13:15:56 |
| Eccentricity: | 0.0101264 |
| inclination: | 98.6290° |
| perigee height: | 679 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 344.6947° |
| argument of perigee: | 249.3345° |
| revolutions per day: | 14.42027888 |
| mean anomaly at epoch: | 109.6964° |
| orbit number at epoch: | 5425 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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