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 25188.89309650 .00007941 00000-0 34417-3 0 9994
2 00022 50.2740 350.3090 0091290 186.2332 173.7496 15.19555949747839
| Epoch (UTC): | 07 July 2025 21:26:03 |
| Eccentricity: | 0.0091290 |
| inclination: | 50.2740° |
| perigee height: | 444 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 350.3090° |
| argument of perigee: | 186.2332° |
| revolutions per day: | 15.19555949 |
| mean anomaly at epoch: | 173.7496° |
| orbit number at epoch: | 74783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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