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 23336.19840392 -.00000070 00000-0 14153-3 0 9999
2 00051 47.2155 40.7423 0107514 316.1477 43.0815 12.18311227818038
| Epoch (UTC): | 02 December 2023 04:45:42 |
| Eccentricity: | 0.0107514 |
| inclination: | 47.2155° |
| perigee height: | 1514 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 40.7423° |
| argument of perigee: | 316.1477° |
| revolutions per day: | 12.18311227 |
| mean anomaly at epoch: | 43.0815° |
| orbit number at epoch: | 81803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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