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 36411U 26145.52501844 +.00000000 +00000-0 +00000-0 0 00005
2 36411 1.2184 83.2434 0005060 32.3600 19.9385 1.00274889 06
| Epoch (UTC): | 25 May 2026 12:36:01 |
| Eccentricity: | 0.0005060 |
| inclination: | 1.2184° |
| perigee height: | 35764 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 83.2434° |
| argument of perigee: | 32.3600° |
| revolutions per day: | 1.00274889 |
| mean anomaly at epoch: | 19.9385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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