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 23271.82064778 .00028913 00000-0 51495-3 0 9997
2 25544 51.6418 175.2116 0005781 68.6872 41.1339 15.49864109417862
| Epoch (UTC): | 28 September 2023 19:41:43 |
| Eccentricity: | 0.0005781 |
| inclination: | 51.6418° |
| perigee height: | 413 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 175.2116° |
| argument of perigee: | 68.6872° |
| revolutions per day: | 15.49864109 |
| mean anomaly at epoch: | 41.1339° |
| orbit number at epoch: | 41786 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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