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 28059U 03049C 25198.51615941 .00000224 00000-0 63353-4 0 9999
2 28059 98.6611 179.6118 0047483 228.5500 131.1613 14.54707759152405
| Epoch (UTC): | 17 July 2025 12:23:16 |
| Eccentricity: | 0.0047483 |
| inclination: | 98.6611° |
| perigee height: | 676 km |
| apogee height: | 744 km |
| right ascension of ascending node: | 179.6118° |
| argument of perigee: | 228.5500° |
| revolutions per day: | 14.54707759 |
| mean anomaly at epoch: | 131.1613° |
| orbit number at epoch: | 15240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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