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 40057U 14034E 25163.52642122 .00003837 00000-0 37333-3 0 9992
2 40057 98.2927 43.2127 0009305 53.7976 306.4101 14.93161529591357
| Epoch (UTC): | 12 June 2025 12:38:02 |
| Eccentricity: | 0.0009305 |
| inclination: | 98.2927° |
| perigee height: | 581 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 43.2127° |
| argument of perigee: | 53.7976° |
| revolutions per day: | 14.93161529 |
| mean anomaly at epoch: | 306.4101° |
| orbit number at epoch: | 59135 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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