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 22590U 93020A 25193.80074169 .00000040 00000-0 25302-4 0 9997
2 22590 82.9302 32.8236 0023503 157.7496 213.1790 13.75599916620129
| Epoch (UTC): | 12 July 2025 19:13:04 |
| Eccentricity: | 0.0023503 |
| inclination: | 82.9302° |
| perigee height: | 962 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 32.8236° |
| argument of perigee: | 157.7496° |
| revolutions per day: | 13.75599916 |
| mean anomaly at epoch: | 213.1790° |
| orbit number at epoch: | 62012 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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