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 23151.68891529 .00000553 00000-0 75973-4 0 9996
2 31598 97.8882 335.4033 0001155 96.6585 263.4760 14.82146704864544
| Epoch (UTC): | 31 May 2023 16:32:02 |
| Eccentricity: | 0.0001155 |
| inclination: | 97.8882° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 335.4033° |
| argument of perigee: | 96.6585° |
| revolutions per day: | 14.82146704 |
| mean anomaly at epoch: | 263.4760° |
| orbit number at epoch: | 86454 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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