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 25774U 99031E 23154.74009793 -.00000111 00000-0 26127-4 0 9997
2 25774 51.5271 279.2644 0374804 45.1396 97.0195 13.46540824179821
| Epoch (UTC): | 03 June 2023 17:45:44 |
| Eccentricity: | 0.0374804 |
| inclination: | 51.5271° |
| perigee height: | 805 km |
| apogee height: | 1365 km |
| right ascension of ascending node: | 279.2644° |
| argument of perigee: | 45.1396° |
| revolutions per day: | 13.46540824 |
| mean anomaly at epoch: | 97.0195° |
| orbit number at epoch: | 17982 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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