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 11165U 26088.18270845 +.00000000 +00000-0 -96643-5 0 00000
2 11165 81.2395 333.9621 0049161 324.2689 35.5196 14.12093899 01
| Epoch (UTC): | 29 March 2026 04:23:06 |
| Eccentricity: | 0.0049161 |
| inclination: | 81.2395° |
| perigee height: | 817 km |
| apogee height: | 888 km |
| right ascension of ascending node: | 333.9621° |
| argument of perigee: | 324.2689° |
| revolutions per day: | 14.12093899 |
| mean anomaly at epoch: | 35.5196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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