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 23180U 26044.67327704 +.00000000 +00000-0 +31523-4 0 00007
2 23180 82.9440 96.6666 0028517 356.2380 118.5254 13.78288742 08
| Epoch (UTC): | 13 February 2026 16:09:31 |
| Eccentricity: | 0.0028517 |
| inclination: | 82.9440° |
| perigee height: | 949 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 96.6666° |
| argument of perigee: | 356.2380° |
| revolutions per day: | 13.78288742 |
| mean anomaly at epoch: | 118.5254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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