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 00051U 60009C 25133.59456860 -.00000097 00000-0 -10575-3 0 9997
2 00051 47.2112 205.8278 0106584 89.4570 271.8430 12.18358636882459
| Epoch (UTC): | 13 May 2025 14:16:10 |
| Eccentricity: | 0.0106584 |
| inclination: | 47.2112° |
| perigee height: | 1514 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 205.8278° |
| argument of perigee: | 89.4570° |
| revolutions per day: | 12.18358636 |
| mean anomaly at epoch: | 271.8430° |
| orbit number at epoch: | 88245 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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