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 56886U 26144.99205765 +.00000000 +00000-0 -45251-4 0 00008
2 56886 43.0042 13.9529 0001181 263.8122 96.2596 15.27582365 03
| Epoch (UTC): | 24 May 2026 23:48:33 |
| Eccentricity: | 0.0001181 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 13.9529° |
| argument of perigee: | 263.8122° |
| revolutions per day: | 15.27582365 |
| mean anomaly at epoch: | 96.2596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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