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 20528U 90023B 25198.49984157 -.00000006 00000-0 -23525-4 0 9992
2 20528 82.9337 41.9785 0033186 99.7722 326.4073 13.73117066769868
| Epoch (UTC): | 17 July 2025 11:59:46 |
| Eccentricity: | 0.0033186 |
| inclination: | 82.9337° |
| perigee height: | 964 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 41.9785° |
| argument of perigee: | 99.7722° |
| revolutions per day: | 13.73117066 |
| mean anomaly at epoch: | 326.4073° |
| orbit number at epoch: | 76986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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