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 25397U 98043D 24261.91031563 .00000398 00000-0 19307-3 0 9996
2 25397 98.9333 230.0663 0000377 196.3590 163.7575 14.24125483360831
| Epoch (UTC): | 17 September 2024 21:50:51 |
| Eccentricity: | 0.0000377 |
| inclination: | 98.9333° |
| perigee height: | 811 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 230.0663° |
| argument of perigee: | 196.3590° |
| revolutions per day: | 14.24125483 |
| mean anomaly at epoch: | 163.7575° |
| orbit number at epoch: | 36083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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