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 23147.77327635 .00000496 00000-0 68940-4 0 9995
2 31598 97.8884 331.5445 0001127 93.7988 266.3354 14.82141760863967
| Epoch (UTC): | 27 May 2023 18:33:31 |
| Eccentricity: | 0.0001127 |
| inclination: | 97.8884° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 331.5445° |
| argument of perigee: | 93.7988° |
| revolutions per day: | 14.82141760 |
| mean anomaly at epoch: | 266.3354° |
| orbit number at epoch: | 86396 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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