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 28521U 05002A 24284.57976035 .00000217 00000-0 16889-3 0 9992
2 28521 82.9499 148.4922 0038852 282.5713 77.1106 13.87813494998595
| Epoch (UTC): | 10 October 2024 13:54:51 |
| Eccentricity: | 0.0038852 |
| inclination: | 82.9499° |
| perigee height: | 908 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 148.4922° |
| argument of perigee: | 282.5713° |
| revolutions per day: | 13.87813494 |
| mean anomaly at epoch: | 77.1106° |
| orbit number at epoch: | 99859 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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