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 56841U 26145.61831204 +.00000000 +00000-0 +36850-4 0 00006
2 56841 43.0035 344.9121 0001839 267.0931 92.9710 15.27578219 09
| Epoch (UTC): | 25 May 2026 14:50:22 |
| Eccentricity: | 0.0001839 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 344.9121° |
| argument of perigee: | 267.0931° |
| revolutions per day: | 15.27578219 |
| mean anomaly at epoch: | 92.9710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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