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 46277U 20061F 24358.17302441 .00014608 00000-0 48059-3 0 9997
2 46277 97.2726 56.8654 0001940 136.5611 223.5784 15.31613387238813
| Epoch (UTC): | 23 December 2024 04:09:09 |
| Eccentricity: | 0.0001940 |
| inclination: | 97.2726° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 56.8654° |
| argument of perigee: | 136.5611° |
| revolutions per day: | 15.31613387 |
| mean anomaly at epoch: | 223.5784° |
| orbit number at epoch: | 23881 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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