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 58238U 26145.46595980 +.00000000 +00000-0 +40130-4 0 00005
2 58238 43.0005 211.8787 0001412 279.2893 80.7799 15.27583668 03
| Epoch (UTC): | 25 May 2026 11:10:58 |
| Eccentricity: | 0.0001412 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.8787° |
| argument of perigee: | 279.2893° |
| revolutions per day: | 15.27583668 |
| mean anomaly at epoch: | 80.7799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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