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 56533U 26145.43578692 +.00000000 +00000-0 +17413-4 0 00007
2 56533 43.0013 124.6287 0000915 264.1083 95.9664 15.27578395 05
| Epoch (UTC): | 25 May 2026 10:27:31 |
| Eccentricity: | 0.0000915 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.6287° |
| argument of perigee: | 264.1083° |
| revolutions per day: | 15.27578395 |
| mean anomaly at epoch: | 95.9664° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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