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 57523U 26145.42054044 +.00000000 +00000-0 +45220-4 0 00003
2 57523 43.0046 288.4837 0001609 265.8778 94.1890 15.27576133 01
| Epoch (UTC): | 25 May 2026 10:05:34 |
| Eccentricity: | 0.0001609 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 288.4837° |
| argument of perigee: | 265.8778° |
| revolutions per day: | 15.27576133 |
| mean anomaly at epoch: | 94.1890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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