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 52565U 26145.35076896 +.00000000 +00000-0 +19111-4 0 00005
2 52565 53.2131 134.9764 0001161 94.6693 265.4432 15.08845314 05
| Epoch (UTC): | 25 May 2026 08:25:06 |
| Eccentricity: | 0.0001161 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 134.9764° |
| argument of perigee: | 94.6693° |
| revolutions per day: | 15.08845314 |
| mean anomaly at epoch: | 265.4432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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