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 52560U 26145.35444822 +.00000000 +00000-0 -40393-4 0 00005
2 52560 53.2123 134.9596 0001172 78.1883 281.9241 15.08845436 00
| Epoch (UTC): | 25 May 2026 08:30:24 |
| Eccentricity: | 0.0001172 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 134.9596° |
| argument of perigee: | 78.1883° |
| revolutions per day: | 15.08845436 |
| mean anomaly at epoch: | 281.9241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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