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 57462U 26145.38524748 +.00000000 +00000-0 +85593-4 0 00000
2 57462 43.0037 263.2319 0001199 254.8315 105.2404 15.27582434 04
| Epoch (UTC): | 25 May 2026 09:14:45 |
| Eccentricity: | 0.0001199 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 263.2319° |
| argument of perigee: | 254.8315° |
| revolutions per day: | 15.27582434 |
| mean anomaly at epoch: | 105.2404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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