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 25567U 26053.57364625 +.00000000 +00000-0 +41112-4 0 00005
2 25567 82.9514 172.3416 0026912 67.2344 308.9633 13.72071952 05
| Epoch (UTC): | 22 February 2026 13:46:03 |
| Eccentricity: | 0.0026912 |
| inclination: | 82.9514° |
| perigee height: | 972 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 172.3416° |
| argument of perigee: | 67.2344° |
| revolutions per day: | 13.72071952 |
| mean anomaly at epoch: | 308.9633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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