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 26145.41962014 +.00000000 +00000-0 +21671-3 0 00006
2 25560 69.8960 286.2245 0008590 280.7601 79.2595 15.09429627 05
| Epoch (UTC): | 25 May 2026 10:04:15 |
| Eccentricity: | 0.0008590 |
| inclination: | 69.8960° |
| perigee height: | 532 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 286.2245° |
| argument of perigee: | 280.7601° |
| revolutions per day: | 15.09429627 |
| mean anomaly at epoch: | 79.2595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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