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 58009U 26145.61615685 +.00000000 +00000-0 +53889-3 0 00007
2 58009 43.0061 352.4047 0000973 269.9058 90.1682 15.27599509 09
| Epoch (UTC): | 25 May 2026 14:47:15 |
| Eccentricity: | 0.0000973 |
| inclination: | 43.0061° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.4047° |
| argument of perigee: | 269.9058° |
| revolutions per day: | 15.27599509 |
| mean anomaly at epoch: | 90.1682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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