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 23271.30279025 .00028951 00000-0 51616-3 0 9990
2 25544 51.6418 177.7770 0005803 66.0906 32.4598 15.49834271417788
| Epoch (UTC): | 28 September 2023 07:16:01 |
| Eccentricity: | 0.0005803 |
| inclination: | 51.6418° |
| perigee height: | 413 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 177.7770° |
| argument of perigee: | 66.0906° |
| revolutions per day: | 15.49834271 |
| mean anomaly at epoch: | 32.4598° |
| orbit number at epoch: | 41778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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