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 23334.68810453 .00026067 00000-0 46332-3 0 9992
2 25544 51.6426 223.8583 0000911 355.2987 98.4937 15.49994401427613
| Epoch (UTC): | 30 November 2023 16:30:52 |
| Eccentricity: | 0.0000911 |
| inclination: | 51.6426° |
| perigee height: | 416 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 223.8583° |
| argument of perigee: | 355.2987° |
| revolutions per day: | 15.49994401 |
| mean anomaly at epoch: | 98.4937° |
| orbit number at epoch: | 42761 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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