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 28886U 05041C 24357.78201523 -.00000016 00000-0 31498-3 0 9997
2 28886 8.1831 42.5957 7175152 335.1135 234.1511 2.24396965157293
| Epoch (UTC): | 22 December 2024 18:46:06 |
| Eccentricity: | 0.7175152 |
| inclination: | 8.1831° |
| perigee height: | 583 km |
| apogee height: | 35949 km |
| right ascension of ascending node: | 42.5957° |
| argument of perigee: | 335.1135° |
| revolutions per day: | 2.24396965 |
| mean anomaly at epoch: | 234.1511° |
| orbit number at epoch: | 15729 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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