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 59332U 26145.42173806 +.00000000 +00000-0 -10124-4 0 00007
2 59332 43.0014 125.0260 0000919 264.8931 95.1816 15.27580987 06
| Epoch (UTC): | 25 May 2026 10:07:18 |
| Eccentricity: | 0.0000919 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 125.0260° |
| argument of perigee: | 264.8931° |
| revolutions per day: | 15.27580987 |
| mean anomaly at epoch: | 95.1816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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