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 17590U 87027B 25144.50265561 .00000158 00000-0 10240-3 0 9996
2 17590 71.0013 165.8544 0006357 222.5360 137.5272 14.17119027974415
| Epoch (UTC): | 24 May 2025 12:03:49 |
| Eccentricity: | 0.0006357 |
| inclination: | 71.0013° |
| perigee height: | 830 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 165.8544° |
| argument of perigee: | 222.5360° |
| revolutions per day: | 14.17119027 |
| mean anomaly at epoch: | 137.5272° |
| orbit number at epoch: | 97441 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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