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 51U 60009C 24257.21776849 -.00000038 00000-0 46211-3 0 9994
2 51 47.2105 235.7897 0105606 87.0655 274.2213 12.18333716852895
| Epoch (UTC): | 13 September 2024 05:13:35 |
| Eccentricity: | 0.0105606 |
| inclination: | 47.2105° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 235.7897° |
| argument of perigee: | 87.0655° |
| revolutions per day: | 12.18333716 |
| mean anomaly at epoch: | 274.2213° |
| orbit number at epoch: | 85289 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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