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 24298U 96051B 25343.79737772 .00000044 00000-0 50352-4 0 9999
2 24298 70.7595 5.5123 0019345 264.9540 94.9371 14.12396273508956
| Epoch (UTC): | 09 December 2025 19:08:13 |
| Eccentricity: | 0.0019345 |
| inclination: | 70.7595° |
| perigee height: | 837 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 5.5123° |
| argument of perigee: | 264.9540° |
| revolutions per day: | 14.12396273 |
| mean anomaly at epoch: | 94.9371° |
| orbit number at epoch: | 50895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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