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 11166U 26137.68618661 +.00000000 +00000-0 -35320-4 0 00007
2 11166 81.2402 230.7006 0065618 350.5885 9.4052 14.14270071 09
| Epoch (UTC): | 17 May 2026 16:28:06 |
| Eccentricity: | 0.0065618 |
| inclination: | 81.2402° |
| perigee height: | 797 km |
| apogee height: | 892 km |
| right ascension of ascending node: | 230.7006° |
| argument of perigee: | 350.5885° |
| revolutions per day: | 14.14270071 |
| mean anomaly at epoch: | 9.4052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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