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 28521U 05002A 23083.44693435 .00000309 00000-0 24587-3 0 9990
2 28521 82.9514 216.5291 0041607 95.9073 264.6835 13.87695851920385
| Epoch (UTC): | 24 March 2023 10:43:35 |
| Eccentricity: | 0.0041607 |
| inclination: | 82.9514° |
| perigee height: | 906 km |
| apogee height: | 967 km |
| right ascension of ascending node: | 216.5291° |
| argument of perigee: | 95.9073° |
| revolutions per day: | 13.87695851 |
| mean anomaly at epoch: | 264.6835° |
| orbit number at epoch: | 92038 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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