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 00050U 60009B 25170.38209033 -.00000068 00000-0 16957-3 0 9999
2 00050 47.2282 207.8521 0112966 13.2089 347.1619 12.20156674893404
| Epoch (UTC): | 19 June 2025 09:10:12 |
| Eccentricity: | 0.0112966 |
| inclination: | 47.2282° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 207.8521° |
| argument of perigee: | 13.2089° |
| revolutions per day: | 12.20156674 |
| mean anomaly at epoch: | 347.1619° |
| orbit number at epoch: | 89340 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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