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 59354U 26145.42303039 +.00000000 +00000-0 +36146-3 0 00004
2 59354 43.0012 186.9008 0001435 277.4617 82.6072 15.27591595 01
| Epoch (UTC): | 25 May 2026 10:09:09 |
| Eccentricity: | 0.0001435 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.9008° |
| argument of perigee: | 277.4617° |
| revolutions per day: | 15.27591595 |
| mean anomaly at epoch: | 82.6072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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