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 42426U 00055TW 24353.88064750 .00005984 00000-0 27933-2 0 9995
2 42426 98.6183 18.2748 0012578 290.7619 69.2210 14.20681226430685
| Epoch (UTC): | 18 December 2024 21:08:07 |
| Eccentricity: | 0.0012578 |
| inclination: | 98.6183° |
| perigee height: | 814 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 18.2748° |
| argument of perigee: | 290.7619° |
| revolutions per day: | 14.20681226 |
| mean anomaly at epoch: | 69.2210° |
| orbit number at epoch: | 43068 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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