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 58252U 26145.23766582 +.00000000 +00000-0 -27592-3 0 00001
2 58252 43.0032 212.7388 0001531 260.1785 99.8894 15.27574043 01
| Epoch (UTC): | 25 May 2026 05:42:14 |
| Eccentricity: | 0.0001531 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 212.7388° |
| argument of perigee: | 260.1785° |
| revolutions per day: | 15.27574043 |
| mean anomaly at epoch: | 99.8894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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