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 39428U 13066N 25138.70978017 .00009780 00000-0 99727-3 0 9991
2 39428 97.8353 56.6101 0087248 72.8866 288.1883 14.88036657615826
| Epoch (UTC): | 18 May 2025 17:02:05 |
| Eccentricity: | 0.0087248 |
| inclination: | 97.8353° |
| perigee height: | 543 km |
| apogee height: | 665 km |
| right ascension of ascending node: | 56.6101° |
| argument of perigee: | 72.8866° |
| revolutions per day: | 14.88036657 |
| mean anomaly at epoch: | 288.1883° |
| orbit number at epoch: | 61582 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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