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 23332.84631098 .00000136 00000-0 81842-4 0 9992
2 58 28.3251 185.2765 0164791 56.1143 305.4961 13.46362611108996
| Epoch (UTC): | 28 November 2023 20:18:41 |
| Eccentricity: | 0.0164791 |
| inclination: | 28.3251° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 185.2765° |
| argument of perigee: | 56.1143° |
| revolutions per day: | 13.46362611 |
| mean anomaly at epoch: | 305.4961° |
| orbit number at epoch: | 10899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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