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 25173.56962280 .00007839 00000-0 34235-3 0 9990
2 00022 50.2746 64.9535 0091747 124.9837 235.9776 15.19297328745501
| Epoch (UTC): | 22 June 2025 13:40:15 |
| Eccentricity: | 0.0091747 |
| inclination: | 50.2746° |
| perigee height: | 445 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 64.9535° |
| argument of perigee: | 124.9837° |
| revolutions per day: | 15.19297328 |
| mean anomaly at epoch: | 235.9776° |
| orbit number at epoch: | 74550 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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