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 13552U 82092A 24278.14223335 .00371200 52360-4 99980-3 0 9994
2 13552 82.5406 125.1701 0004602 273.6765 86.3984 15.94294292305865
| Epoch (UTC): | 04 October 2024 03:24:48 |
| Eccentricity: | 0.0004602 |
| inclination: | 82.5406° |
| perigee height: | 287 km |
| apogee height: | 293 km |
| right ascension of ascending node: | 125.1701° |
| argument of perigee: | 273.6765° |
| revolutions per day: | 15.94294292 |
| mean anomaly at epoch: | 86.3984° |
| orbit number at epoch: | 30586 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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