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 25544U 26022.94831486 +.00000000 +00000-0 +24973-3 0 00006
2 25544 51.6328 298.4677 0007749 48.1765 311.9884 15.49569219 03
| Epoch (UTC): | 22 January 2026 22:45:34 |
| Eccentricity: | 0.0007749 |
| inclination: | 51.6328° |
| perigee height: | 413 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 298.4677° |
| argument of perigee: | 48.1765° |
| revolutions per day: | 15.49569219 |
| mean anomaly at epoch: | 311.9884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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