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 52274U 26145.38112802 +.00000000 +00000-0 +34395-4 0 00004
2 52274 53.2137 124.8367 0001284 82.9273 277.1865 15.08840594 00
| Epoch (UTC): | 25 May 2026 09:08:49 |
| Eccentricity: | 0.0001284 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 124.8367° |
| argument of perigee: | 82.9273° |
| revolutions per day: | 15.08840594 |
| mean anomaly at epoch: | 277.1865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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