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 54838U 26145.47091779 +.00000000 +00000-0 +24852-4 0 00008
2 54838 43.0044 59.2397 0001197 275.3849 84.6866 15.27588858 01
| Epoch (UTC): | 25 May 2026 11:18:07 |
| Eccentricity: | 0.0001197 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 59.2397° |
| argument of perigee: | 275.3849° |
| revolutions per day: | 15.27588858 |
| mean anomaly at epoch: | 84.6866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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