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 23339.15134521 -.00000057 00000-0 26712-3 0 9997
2 51 47.2155 31.6067 0107666 324.8913 34.4814 12.18311293818384
| Epoch (UTC): | 05 December 2023 03:37:56 |
| Eccentricity: | 0.0107666 |
| inclination: | 47.2155° |
| perigee height: | 1514 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 31.6067° |
| argument of perigee: | 324.8913° |
| revolutions per day: | 12.18311293 |
| mean anomaly at epoch: | 34.4814° |
| orbit number at epoch: | 81838 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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