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 25136.87544599 -.00000081 00000-0 48210-4 0 9998
2 00051 47.2109 195.6758 0106472 99.2203 262.0645 12.18358612882850
| Epoch (UTC): | 16 May 2025 21:00:38 |
| Eccentricity: | 0.0106472 |
| inclination: | 47.2109° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 195.6758° |
| argument of perigee: | 99.2203° |
| revolutions per day: | 12.18358612 |
| mean anomaly at epoch: | 262.0645° |
| orbit number at epoch: | 88285 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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