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 31598U 07023A 23152.16149142 .00000585 00000-0 80105-4 0 9995
2 31598 97.8882 335.8690 0001158 97.0485 263.0859 14.82147464864611
| Epoch (UTC): | 01 June 2023 03:52:32 |
| Eccentricity: | 0.0001158 |
| inclination: | 97.8882° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 335.8690° |
| argument of perigee: | 97.0485° |
| revolutions per day: | 14.82147464 |
| mean anomaly at epoch: | 263.0859° |
| orbit number at epoch: | 86461 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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