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 25544U 98067A 23080.38988954 .00015304 00000-0 28187-3 0 9999
2 25544 51.6415 43.5078 0006133 115.2181 346.9578 15.49345862388179
| Epoch (UTC): | 21 March 2023 09:21:26 |
| Eccentricity: | 0.0006133 |
| inclination: | 51.6415° |
| perigee height: | 414 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 43.5078° |
| argument of perigee: | 115.2181° |
| revolutions per day: | 15.49345862 |
| mean anomaly at epoch: | 346.9578° |
| orbit number at epoch: | 38817 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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