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 51896U 26145.65992170 +.00000000 +00000-0 -10841-3 0 00007
2 51896 53.2149 13.8073 0001256 74.4138 285.6993 15.08840866 06
| Epoch (UTC): | 25 May 2026 15:50:17 |
| Eccentricity: | 0.0001256 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 13.8073° |
| argument of perigee: | 74.4138° |
| revolutions per day: | 15.08840866 |
| mean anomaly at epoch: | 285.6993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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