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 59250U 26145.04644961 +.00000000 +00000-0 +19453-4 0 00002
2 59250 43.0015 61.0815 0001192 267.5824 92.4892 15.27575775 09
| Epoch (UTC): | 25 May 2026 01:06:53 |
| Eccentricity: | 0.0001192 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 61.0815° |
| argument of perigee: | 267.5824° |
| revolutions per day: | 15.27575775 |
| mean anomaly at epoch: | 92.4892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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