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 00058U 60013A 24357.48692440 .00000119 00000-0 55969-4 0 9990
2 00058 28.3293 8.3493 0164934 42.3110 319.0030 13.46398899161001
| Epoch (UTC): | 22 December 2024 11:41:10 |
| Eccentricity: | 0.0164934 |
| inclination: | 28.3293° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 8.3493° |
| argument of perigee: | 42.3110° |
| revolutions per day: | 13.46398899 |
| mean anomaly at epoch: | 319.0030° |
| orbit number at epoch: | 16100 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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