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 32258U 07046A 23088.38729907 .00000034 00000-0 00000-0 0 9990
2 32258 0.0168 159.1520 0000596 173.8401 358.9434 1.00272251 40554
| Epoch (UTC): | 29 March 2023 09:17:42 |
| Eccentricity: | 0.0000596 |
| inclination: | 0.0168° |
| perigee height: | 35783 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 159.1520° |
| argument of perigee: | 173.8401° |
| revolutions per day: | 1.00272251 |
| mean anomaly at epoch: | 358.9434° |
| orbit number at epoch: | 4055 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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