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 52264U 26145.34800867 +.00000000 +00000-0 +80723-4 0 00000
2 52264 53.2123 124.9837 0001364 87.8187 272.2961 15.08833902 02
| Epoch (UTC): | 25 May 2026 08:21:07 |
| Eccentricity: | 0.0001364 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 124.9837° |
| argument of perigee: | 87.8187° |
| revolutions per day: | 15.08833902 |
| mean anomaly at epoch: | 272.2961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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