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 26241U 99057EF 25346.97299692 .00000529 00000-0 19210-3 0 9990
2 26241 98.9070 356.5011 0107946 217.0299 202.4290 14.34493951344988
| Epoch (UTC): | 12 December 2025 23:21:06 |
| Eccentricity: | 0.0107946 |
| inclination: | 98.9070° |
| perigee height: | 699 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 356.5011° |
| argument of perigee: | 217.0299° |
| revolutions per day: | 14.34493951 |
| mean anomaly at epoch: | 202.4290° |
| orbit number at epoch: | 34498 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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