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 23036.22173786 .00010856 00000-0 20054-3 0 9994
2 25544 51.6426 262.1755 0008177 315.4619 200.8788 15.49603028381324
| Epoch (UTC): | 05 February 2023 05:19:18 |
| Eccentricity: | 0.0008177 |
| inclination: | 51.6426° |
| perigee height: | 412 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 262.1755° |
| argument of perigee: | 315.4619° |
| revolutions per day: | 15.49603028 |
| mean anomaly at epoch: | 200.8788° |
| orbit number at epoch: | 38132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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