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 05918U 72022B 25193.85863624 -.00000072 00000-0 -50482-4 0 9992
2 05918 81.2390 353.9676 0057107 323.8792 35.8524 14.06248950731929
| Epoch (UTC): | 12 July 2025 20:36:26 |
| Eccentricity: | 0.0057107 |
| inclination: | 81.2390° |
| perigee height: | 831 km |
| apogee height: | 913 km |
| right ascension of ascending node: | 353.9676° |
| argument of perigee: | 323.8792° |
| revolutions per day: | 14.06248950 |
| mean anomaly at epoch: | 35.8524° |
| orbit number at epoch: | 73192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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