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 23333.49240814 .00000268 00000-0 13661-3 0 9992
2 25397 98.8936 292.5593 0001963 49.8058 310.3291 14.23949414319079
| Epoch (UTC): | 29 November 2023 11:49:04 |
| Eccentricity: | 0.0001963 |
| inclination: | 98.8936° |
| perigee height: | 810 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 292.5593° |
| argument of perigee: | 49.8058° |
| revolutions per day: | 14.23949414 |
| mean anomaly at epoch: | 310.3291° |
| orbit number at epoch: | 31907 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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