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 59525U 26145.62207957 +.00000000 +00000-0 +12407-3 0 00002
2 59525 43.0003 243.3561 0001075 270.8337 89.2392 15.27578659 03
| Epoch (UTC): | 25 May 2026 14:55:47 |
| Eccentricity: | 0.0001075 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 243.3561° |
| argument of perigee: | 270.8337° |
| revolutions per day: | 15.27578659 |
| mean anomaly at epoch: | 89.2392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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