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 58404U 26145.52189844 +.00000000 +00000-0 +76533-4 0 00001
2 58404 43.0066 338.8918 0002338 267.7447 92.3137 15.27573829 09
| Epoch (UTC): | 25 May 2026 12:31:32 |
| Eccentricity: | 0.0002338 |
| inclination: | 43.0066° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 338.8918° |
| argument of perigee: | 267.7447° |
| revolutions per day: | 15.27573829 |
| mean anomaly at epoch: | 92.3137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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