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 59357U 26145.54381194 +.00000000 +00000-0 +13188-3 0 00009
2 59357 43.0017 181.7312 0001191 267.6294 92.4421 15.27602689 05
| Epoch (UTC): | 25 May 2026 13:03:05 |
| Eccentricity: | 0.0001191 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 181.7312° |
| argument of perigee: | 267.6294° |
| revolutions per day: | 15.27602689 |
| mean anomaly at epoch: | 92.4421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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