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 23332.59115930 .00073773 00000-0 11434-2 0 9999
2 47311 60.6736 141.0029 0022693 37.9824 322.2872 15.53238047159681
| Epoch (UTC): | 28 November 2023 14:11:16 |
| Eccentricity: | 0.0022693 |
| inclination: | 60.6736° |
| perigee height: | 392 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 141.0029° |
| argument of perigee: | 37.9824° |
| revolutions per day: | 15.53238047 |
| mean anomaly at epoch: | 322.2872° |
| orbit number at epoch: | 15968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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