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 23081.87225215 .00015935 00000-0 29262-3 0 9993
2 25544 51.6418 36.1698 0006055 120.4003 335.4746 15.49396602388406
| Epoch (UTC): | 22 March 2023 20:56:02 |
| Eccentricity: | 0.0006055 |
| inclination: | 51.6418° |
| perigee height: | 414 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 36.1698° |
| argument of perigee: | 120.4003° |
| revolutions per day: | 15.49396602 |
| mean anomaly at epoch: | 335.4746° |
| orbit number at epoch: | 38840 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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