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 23333.94288802 .00082113 00000-0 12600-2 0 9992
2 47311 60.6746 135.6916 0023098 38.0034 322.2692 15.53459724159903
| Epoch (UTC): | 29 November 2023 22:37:45 |
| Eccentricity: | 0.0023098 |
| inclination: | 60.6746° |
| perigee height: | 391 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 135.6916° |
| argument of perigee: | 38.0034° |
| revolutions per day: | 15.53459724 |
| mean anomaly at epoch: | 322.2692° |
| orbit number at epoch: | 15990 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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