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 41054U 00055M 24357.81706130 .00002801 00000-0 10423-2 0 9994
2 41054 99.0652 210.7087 0065733 270.8460 88.5191 14.31727625472949
| Epoch (UTC): | 22 December 2024 19:36:34 |
| Eccentricity: | 0.0065733 |
| inclination: | 99.0652° |
| perigee height: | 739 km |
| apogee height: | 833 km |
| right ascension of ascending node: | 210.7087° |
| argument of perigee: | 270.8460° |
| revolutions per day: | 14.31727625 |
| mean anomaly at epoch: | 88.5191° |
| orbit number at epoch: | 47294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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