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 52604U 26145.42804573 +.00000000 +00000-0 +41115-4 0 00007
2 52604 53.2146 294.6265 0001422 93.9084 266.2071 15.08840369 04
| Epoch (UTC): | 25 May 2026 10:16:23 |
| Eccentricity: | 0.0001422 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 294.6265° |
| argument of perigee: | 93.9084° |
| revolutions per day: | 15.08840369 |
| mean anomaly at epoch: | 266.2071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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