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 57965U 26145.38649972 +.00000000 +00000-0 +88987-4 0 00005
2 57965 43.0025 263.0917 0001966 265.5825 94.4802 15.27585807 06
| Epoch (UTC): | 25 May 2026 09:16:33 |
| Eccentricity: | 0.0001966 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 263.0917° |
| argument of perigee: | 265.5825° |
| revolutions per day: | 15.27585807 |
| mean anomaly at epoch: | 94.4802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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