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 26088.02150397 +.00000000 +00000-0 +32696-4 0 00009
2 11166 81.2356 279.4170 0066644 130.6519 230.0475 14.14262328 07
| Epoch (UTC): | 29 March 2026 00:30:57 |
| Eccentricity: | 0.0066644 |
| inclination: | 81.2356° |
| perigee height: | 797 km |
| apogee height: | 893 km |
| right ascension of ascending node: | 279.4170° |
| argument of perigee: | 130.6519° |
| revolutions per day: | 14.14262328 |
| mean anomaly at epoch: | 230.0475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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