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 59469U 26145.53235000 +.00000000 +00000-0 +20310-3 0 00001
2 59469 43.0035 317.1946 0001799 270.2386 89.8260 15.27582589 00
| Epoch (UTC): | 25 May 2026 12:46:35 |
| Eccentricity: | 0.0001799 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.1946° |
| argument of perigee: | 270.2386° |
| revolutions per day: | 15.27582589 |
| mean anomaly at epoch: | 89.8260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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