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 51805U 26145.59641748 +.00000000 +00000-0 +10363-3 0 00000
2 51805 53.2116 343.9495 0001284 87.3979 272.7160 15.08839518 07
| Epoch (UTC): | 25 May 2026 14:18:50 |
| Eccentricity: | 0.0001284 |
| inclination: | 53.2116° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 343.9495° |
| argument of perigee: | 87.3979° |
| revolutions per day: | 15.08839518 |
| mean anomaly at epoch: | 272.7160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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