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 00022U 59009A 25173.89848066 .00007825 00000-0 34170-3 0 9994
2 00022 50.2749 63.3518 0091749 126.2970 234.6504 15.19302848745557
| Epoch (UTC): | 22 June 2025 21:33:48 |
| Eccentricity: | 0.0091749 |
| inclination: | 50.2749° |
| perigee height: | 445 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 63.3518° |
| argument of perigee: | 126.2970° |
| revolutions per day: | 15.19302848 |
| mean anomaly at epoch: | 234.6504° |
| orbit number at epoch: | 74555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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