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 57521U 26145.40640892 +.00000000 +00000-0 +10210-4 0 00002
2 57521 43.0035 288.3837 0001570 270.9629 89.1043 15.27591932 03
| Epoch (UTC): | 25 May 2026 09:45:13 |
| Eccentricity: | 0.0001570 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 288.3837° |
| argument of perigee: | 270.9629° |
| revolutions per day: | 15.27591932 |
| mean anomaly at epoch: | 89.1043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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