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 11085U 26065.20873609 +.00000000 +00000-0 -27664-3 0 00001
2 11085 82.5438 104.6941 0013273 178.7795 247.3367 11.96568210 03
| Epoch (UTC): | 06 March 2026 05:00:34 |
| Eccentricity: | 0.0013273 |
| inclination: | 82.5438° |
| perigee height: | 1686 km |
| apogee height: | 1707 km |
| right ascension of ascending node: | 104.6941° |
| argument of perigee: | 178.7795° |
| revolutions per day: | 11.96568210 |
| mean anomaly at epoch: | 247.3367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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