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 57524U 26145.66409919 +.00000000 +00000-0 +72789-4 0 00005
2 57524 43.0024 286.8936 0002136 267.9080 92.1527 15.27577797 07
| Epoch (UTC): | 25 May 2026 15:56:18 |
| Eccentricity: | 0.0002136 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 286.8936° |
| argument of perigee: | 267.9080° |
| revolutions per day: | 15.27577797 |
| mean anomaly at epoch: | 92.1527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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