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 25138.70272265 .00008869 00000-0 39123-3 0 9999
2 00022 50.2741 234.6938 0092899 346.4059 13.4398 15.18679682740202
| Epoch (UTC): | 18 May 2025 16:51:55 |
| Eccentricity: | 0.0092899 |
| inclination: | 50.2741° |
| perigee height: | 446 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 234.6938° |
| argument of perigee: | 346.4059° |
| revolutions per day: | 15.18679682 |
| mean anomaly at epoch: | 13.4398° |
| orbit number at epoch: | 74020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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