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 25560U 26116.39230536 +.00000000 +00000-0 +29985-3 0 00004
2 25560 69.8979 1.0525 0007296 311.5606 48.4931 15.09259152 05
| Epoch (UTC): | 26 April 2026 09:24:55 |
| Eccentricity: | 0.0007296 |
| inclination: | 69.8979° |
| perigee height: | 533 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 1.0525° |
| argument of perigee: | 311.5606° |
| revolutions per day: | 15.09259152 |
| mean anomaly at epoch: | 48.4931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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