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 25082.88566696 .00000200 00000-0 15379-3 0 9996
2 28521 82.9530 24.2111 0040227 171.4204 188.7656 13.87861656 21355
| Epoch (UTC): | 23 March 2025 21:15:21 |
| Eccentricity: | 0.0040227 |
| inclination: | 82.9530° |
| perigee height: | 907 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 24.2111° |
| argument of perigee: | 171.4204° |
| revolutions per day: | 13.87861656 |
| mean anomaly at epoch: | 188.7656° |
| orbit number at epoch: | 2135 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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