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 20559U 90030B 25198.33669525 .00098935 00000-0 12928-2 0 9995
2 20559 30.7982 275.2456 4343578 9.6814 356.5662 6.92425624493240
| Epoch (UTC): | 17 July 2025 08:04:50 |
| Eccentricity: | 0.4343578 |
| inclination: | 30.7982° |
| perigee height: | 199 km |
| apogee height: | 10300 km |
| right ascension of ascending node: | 275.2456° |
| argument of perigee: | 9.6814° |
| revolutions per day: | 6.92425624 |
| mean anomaly at epoch: | 356.5662° |
| orbit number at epoch: | 49324 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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