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 42568U 72058KB 23334.25896699 .00001409 00000-0 70221-3 0 9995
2 42568 98.9908 337.8803 0028536 14.6460 345.5535 14.18381881958844
| Epoch (UTC): | 30 November 2023 06:12:54 |
| Eccentricity: | 0.0028536 |
| inclination: | 98.9908° |
| perigee height: | 810 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 337.8803° |
| argument of perigee: | 14.6460° |
| revolutions per day: | 14.18381881 |
| mean anomaly at epoch: | 345.5535° |
| orbit number at epoch: | 95884 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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