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 52564U 26145.33379944 +.00000000 +00000-0 +19325-4 0 00009
2 52564 53.2121 150.0608 0001155 60.5620 299.5487 15.08836476 01
| Epoch (UTC): | 25 May 2026 08:00:40 |
| Eccentricity: | 0.0001155 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 150.0608° |
| argument of perigee: | 60.5620° |
| revolutions per day: | 15.08836476 |
| mean anomaly at epoch: | 299.5487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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