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 24971U 97057A 25343.46785855 .00000410 00000-0 15626-3 0 9994
2 24971 98.8291 328.2736 0053156 66.9123 293.7653 14.35409198475397
| Epoch (UTC): | 09 December 2025 11:13:42 |
| Eccentricity: | 0.0053156 |
| inclination: | 98.8291° |
| perigee height: | 735 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 328.2736° |
| argument of perigee: | 66.9123° |
| revolutions per day: | 14.35409198 |
| mean anomaly at epoch: | 293.7653° |
| orbit number at epoch: | 47539 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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