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 51125U 26145.45661058 +.00000000 +00000-0 -45851-5 0 00009
2 51125 53.2119 314.5085 0001198 92.2834 267.8295 15.08832479 06
| Epoch (UTC): | 25 May 2026 10:57:31 |
| Eccentricity: | 0.0001198 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 314.5085° |
| argument of perigee: | 92.2834° |
| revolutions per day: | 15.08832479 |
| mean anomaly at epoch: | 267.8295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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