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 58225U 26145.55386625 +.00000000 +00000-0 +54271-5 0 00007
2 58225 43.0025 338.2236 0001324 273.7870 86.2831 15.27590609 01
| Epoch (UTC): | 25 May 2026 13:17:34 |
| Eccentricity: | 0.0001324 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.2236° |
| argument of perigee: | 273.7870° |
| revolutions per day: | 15.27590609 |
| mean anomaly at epoch: | 86.2831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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