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 54873U 26145.41710174 +.00000000 +00000-0 +14814-4 0 00005
2 54873 43.0029 48.3746 0001063 251.7359 108.3378 15.27576502 01
| Epoch (UTC): | 25 May 2026 10:00:37 |
| Eccentricity: | 0.0001063 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.3746° |
| argument of perigee: | 251.7359° |
| revolutions per day: | 15.27576502 |
| mean anomaly at epoch: | 108.3378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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