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 28523U 05002C 23342.55191539 .00000140 00000-0 10405-3 0 9997
2 28523 82.9507 22.6823 0039267 87.2369 273.3287 13.87733724956106
| Epoch (UTC): | 08 December 2023 13:14:45 |
| Eccentricity: | 0.0039267 |
| inclination: | 82.9507° |
| perigee height: | 908 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 22.6823° |
| argument of perigee: | 87.2369° |
| revolutions per day: | 13.87733724 |
| mean anomaly at epoch: | 273.3287° |
| orbit number at epoch: | 95610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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