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 26100.19015079 +.00000000 +00000-0 +36437-4 0 00006
2 11166 81.2362 267.4774 0066929 96.4339 264.4461 14.14265761 06
| Epoch (UTC): | 10 April 2026 04:33:49 |
| Eccentricity: | 0.0066929 |
| inclination: | 81.2362° |
| perigee height: | 796 km |
| apogee height: | 893 km |
| right ascension of ascending node: | 267.4774° |
| argument of perigee: | 96.4339° |
| revolutions per day: | 14.14265761 |
| mean anomaly at epoch: | 264.4461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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