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 59358U 26145.44857708 +.00000000 +00000-0 -11038-4 0 00002
2 59358 43.0024 186.2320 0001450 273.3644 86.7042 15.27568459 05
| Epoch (UTC): | 25 May 2026 10:45:57 |
| Eccentricity: | 0.0001450 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.2320° |
| argument of perigee: | 273.3644° |
| revolutions per day: | 15.27568459 |
| mean anomaly at epoch: | 86.7042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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