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 23334.55437867 .00029312 00000-0 51978-3 0 9990
2 25544 51.6423 224.5224 0001078 355.3671 71.7567 15.49994850427594
| Epoch (UTC): | 30 November 2023 13:18:18 |
| Eccentricity: | 0.0001078 |
| inclination: | 51.6423° |
| perigee height: | 416 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 224.5224° |
| argument of perigee: | 355.3671° |
| revolutions per day: | 15.49994850 |
| mean anomaly at epoch: | 71.7567° |
| orbit number at epoch: | 42759 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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