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 59236U 26145.66668980 +.00000000 +00000-0 +77649-3 0 00001
2 59236 43.0003 356.3464 0001928 267.5013 26.4252 15.32899832 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001928 |
| inclination: | 43.0003° |
| perigee height: | 466 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 356.3464° |
| argument of perigee: | 267.5013° |
| revolutions per day: | 15.32899832 |
| mean anomaly at epoch: | 26.4252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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