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 23333.58785172 .00023126 00000-0 41302-3 0 9994
2 25544 51.6431 229.3060 0000955 349.0691 81.3873 15.49930125427445
| Epoch (UTC): | 29 November 2023 14:06:30 |
| Eccentricity: | 0.0000955 |
| inclination: | 51.6431° |
| perigee height: | 416 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 229.3060° |
| argument of perigee: | 349.0691° |
| revolutions per day: | 15.49930125 |
| mean anomaly at epoch: | 81.3873° |
| orbit number at epoch: | 42744 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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