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 41522U 00055MW 24356.37930136 .00079173 00000-0 12735-1 0 9992
2 41522 98.8585 144.9294 0018981 231.6658 128.2840 14.70988920450990
| Epoch (UTC): | 21 December 2024 09:06:11 |
| Eccentricity: | 0.0018981 |
| inclination: | 98.8585° |
| perigee height: | 644 km |
| apogee height: | 671 km |
| right ascension of ascending node: | 144.9294° |
| argument of perigee: | 231.6658° |
| revolutions per day: | 14.70988920 |
| mean anomaly at epoch: | 128.2840° |
| orbit number at epoch: | 45099 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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