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 55828U 23029AJ 24357.58881558 .00000034 00000-0 50520-4 0 9996
2 55828 87.9254 22.2031 0002566 87.7362 272.4065 13.20770830 89652
| Epoch (UTC): | 22 December 2024 14:07:53 |
| Eccentricity: | 0.0002566 |
| inclination: | 87.9254° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 22.2031° |
| argument of perigee: | 87.7362° |
| revolutions per day: | 13.20770830 |
| mean anomaly at epoch: | 272.4065° |
| orbit number at epoch: | 8965 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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