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 58248U 26145.44925707 +.00000000 +00000-0 +11984-3 0 00002
2 58248 43.0037 211.7492 0002071 270.0185 90.0429 15.27579360 04
| Epoch (UTC): | 25 May 2026 10:46:55 |
| Eccentricity: | 0.0002071 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.7492° |
| argument of perigee: | 270.0185° |
| revolutions per day: | 15.27579360 |
| mean anomaly at epoch: | 90.0429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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