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 is defined by the following mean orbital elements,
1 57490U 26145.63668882 +.00000000 +00000-0 +37678-4 0 00008
2 57490 98.6841 216.0645 0001447 109.8726 250.2607 14.19934554 03
| Epoch (UTC): | 25 May 2026 15:16:49 |
| Eccentricity: | 0.0001447 |
| inclination: | 98.6841° |
| perigee height: | 825 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 216.0645° |
| argument of perigee: | 109.8726° |
| revolutions per day: | 14.19934554 |
| mean anomaly at epoch: | 250.2607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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