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 54805U 26145.13276446 +.00000000 +00000-0 +26172-3 0 00007
2 54805 53.2188 45.6832 0001377 96.0672 264.0477 15.07992879 04
| Epoch (UTC): | 25 May 2026 03:11:10 |
| Eccentricity: | 0.0001377 |
| inclination: | 53.2188° |
| perigee height: | 541 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 45.6832° |
| argument of perigee: | 96.0672° |
| revolutions per day: | 15.07992879 |
| mean anomaly at epoch: | 264.0477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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