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 52601U 26145.37285037 +.00000000 +00000-0 -19256-4 0 00008
2 52601 53.2138 294.8741 0001497 87.5507 272.5657 15.08836689 04
| Epoch (UTC): | 25 May 2026 08:56:54 |
| Eccentricity: | 0.0001497 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 294.8741° |
| argument of perigee: | 87.5507° |
| revolutions per day: | 15.08836689 |
| mean anomaly at epoch: | 272.5657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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