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 24254.67502934 -.00000008 00000-0 75626-3 0 9992
2 00051 47.2104 243.6578 0105572 79.5153 281.7511 12.18333310852590
| Epoch (UTC): | 10 September 2024 16:12:02 |
| Eccentricity: | 0.0105572 |
| inclination: | 47.2104° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 243.6578° |
| argument of perigee: | 79.5153° |
| revolutions per day: | 12.18333310 |
| mean anomaly at epoch: | 281.7511° |
| orbit number at epoch: | 85259 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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