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 47311U 21002C 23265.91219863 .00049582 00000-0 10382-2 0 9992
2 47311 60.6795 41.2785 0013977 352.7311 7.3581 15.45007086149360
| Epoch (UTC): | 22 September 2023 21:53:33 |
| Eccentricity: | 0.0013977 |
| inclination: | 60.6795° |
| perigee height: | 422 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 41.2785° |
| argument of perigee: | 352.7311° |
| revolutions per day: | 15.45007086 |
| mean anomaly at epoch: | 7.3581° |
| orbit number at epoch: | 14936 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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