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 23156.54967602 .00000553 00000-0 76035-4 0 9992
2 31598 97.8881 340.1934 0001209 99.3041 260.8309 14.82155918865181
| Epoch (UTC): | 05 June 2023 13:11:32 |
| Eccentricity: | 0.0001209 |
| inclination: | 97.8881° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 340.1934° |
| argument of perigee: | 99.3041° |
| revolutions per day: | 14.82155918 |
| mean anomaly at epoch: | 260.8309° |
| orbit number at epoch: | 86518 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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