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 55179U 26145.33350110 +.00000000 +00000-0 +58879-4 0 00005
2 55179 87.9162 10.3797 0001935 79.2676 280.8673 13.17649907 05
| Epoch (UTC): | 25 May 2026 08:00:14 |
| Eccentricity: | 0.0001935 |
| inclination: | 87.9162° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3797° |
| argument of perigee: | 79.2676° |
| revolutions per day: | 13.17649907 |
| mean anomaly at epoch: | 280.8673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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