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 24283.83066806 .00000659 00000-0 30639-3 0 9990
2 25397 98.9378 252.3493 0001573 142.1301 217.9988 14.24148984363739
| Epoch (UTC): | 09 October 2024 19:56:09 |
| Eccentricity: | 0.0001573 |
| inclination: | 98.9378° |
| perigee height: | 810 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 252.3493° |
| argument of perigee: | 142.1301° |
| revolutions per day: | 14.24148984 |
| mean anomaly at epoch: | 217.9988° |
| orbit number at epoch: | 36373 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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