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 23083.67246850 .00018332 00000-0 33443-3 0 9991
2 25544 51.6427 27.2602 0006167 127.6308 296.4423 15.49470984388687
| Epoch (UTC): | 24 March 2023 16:08:21 |
| Eccentricity: | 0.0006167 |
| inclination: | 51.6427° |
| perigee height: | 414 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 27.2602° |
| argument of perigee: | 127.6308° |
| revolutions per day: | 15.49470984 |
| mean anomaly at epoch: | 296.4423° |
| orbit number at epoch: | 38868 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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