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 58U 60013A 23272.78602147 .00000118 00000-0 47449-4 0 9996
2 58 28.3271 129.9942 0164979 278.8231 79.3666 13.46358861100891
| Epoch (UTC): | 29 September 2023 18:51:52 |
| Eccentricity: | 0.0164979 |
| inclination: | 28.3271° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 129.9942° |
| argument of perigee: | 278.8231° |
| revolutions per day: | 13.46358861 |
| mean anomaly at epoch: | 79.3666° |
| orbit number at epoch: | 10089 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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