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 52159U 22033C 25136.44215132 .00000552 00000-0 89639-4 0 9992
2 52159 97.9785 219.3854 0001441 91.2814 268.8560 14.74937976168171
| Epoch (UTC): | 16 May 2025 10:36:41 |
| Eccentricity: | 0.0001441 |
| inclination: | 97.9785° |
| perigee height: | 644 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 219.3854° |
| argument of perigee: | 91.2814° |
| revolutions per day: | 14.74937976 |
| mean anomaly at epoch: | 268.8560° |
| orbit number at epoch: | 16817 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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