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 26042.11518432 +.00000000 +00000-0 +29174-4 0 00003
2 23180 82.9445 98.5718 0028717 3.4129 25.6831 13.78288696 03
| Epoch (UTC): | 11 February 2026 02:45:51 |
| Eccentricity: | 0.0028717 |
| inclination: | 82.9445° |
| perigee height: | 949 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 98.5718° |
| argument of perigee: | 3.4129° |
| revolutions per day: | 13.78288696 |
| mean anomaly at epoch: | 25.6831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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