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 56013U 26144.97092925 +.00000000 +00000-0 +22005-4 0 00001
2 56013 43.0037 348.9724 0001764 258.2028 101.8626 15.27577131 09
| Epoch (UTC): | 24 May 2026 23:18:08 |
| Eccentricity: | 0.0001764 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 348.9724° |
| argument of perigee: | 258.2028° |
| revolutions per day: | 15.27577131 |
| mean anomaly at epoch: | 101.8626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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