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 09572U 75112C 23027.74005370 .00041725 00000-0 17827-2 0 9995
2 09572 74.0248 141.4874 0006817 30.0123 330.1465 15.22649065515610
| Epoch (UTC): | 27 January 2023 17:45:40 |
| Eccentricity: | 0.0006817 |
| inclination: | 74.0248° |
| perigee height: | 493 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 141.4874° |
| argument of perigee: | 30.0123° |
| revolutions per day: | 15.22649065 |
| mean anomaly at epoch: | 330.1465° |
| orbit number at epoch: | 51561 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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