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 11080U 26150.60479804 +.00000000 +00000-0 +37518-4 0 00003
2 11080 99.4724 34.6705 0008358 323.0300 37.0277 13.84516335 02
| Epoch (UTC): | 30 May 2026 14:30:54 |
| Eccentricity: | 0.0008358 |
| inclination: | 99.4724° |
| perigee height: | 942 km |
| apogee height: | 954 km |
| right ascension of ascending node: | 34.6705° |
| argument of perigee: | 323.0300° |
| revolutions per day: | 13.84516335 |
| mean anomaly at epoch: | 37.0277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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