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 59502U 26145.40148419 +.00000000 +00000-0 -19135-4 0 00007
2 59502 43.0025 266.8652 0001948 288.0275 72.0364 15.27574858 00
| Epoch (UTC): | 25 May 2026 09:38:08 |
| Eccentricity: | 0.0001948 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.8652° |
| argument of perigee: | 288.0275° |
| revolutions per day: | 15.27574858 |
| mean anomaly at epoch: | 72.0364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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