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 08800U 76032B 25347.68598684 -.00000099 00000-0 -60399-4 0 9990
2 08800 81.2510 79.2662 0094483 42.4975 318.3459 14.10631404555121
| Epoch (UTC): | 13 December 2025 16:27:49 |
| Eccentricity: | 0.0094483 |
| inclination: | 81.2510° |
| perigee height: | 789 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 79.2662° |
| argument of perigee: | 42.4975° |
| revolutions per day: | 14.10631404 |
| mean anomaly at epoch: | 318.3459° |
| orbit number at epoch: | 55512 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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