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 25399U 98043F 25080.48670364 .00000513 00000-0 23683-3 0 9999
2 25399 98.9259 53.1601 0001779 15.3131 344.8101 14.25426549386837
| Epoch (UTC): | 21 March 2025 11:40:51 |
| Eccentricity: | 0.0001779 |
| inclination: | 98.9259° |
| perigee height: | 806 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 53.1601° |
| argument of perigee: | 15.3131° |
| revolutions per day: | 14.25426549 |
| mean anomaly at epoch: | 344.8101° |
| orbit number at epoch: | 38683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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