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 11060U 26070.92645841 +.00000000 +00000-0 +10312-3 0 00005
2 11060 98.4631 96.3471 0010863 158.9671 201.1955 14.19339385 05
| Epoch (UTC): | 11 March 2026 22:14:06 |
| Eccentricity: | 0.0010863 |
| inclination: | 98.4631° |
| perigee height: | 820 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 96.3471° |
| argument of perigee: | 158.9671° |
| revolutions per day: | 14.19339385 |
| mean anomaly at epoch: | 201.1955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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