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 58241U 26145.52363600 +.00000000 +00000-0 +27148-4 0 00002
2 58241 43.0004 211.4387 0001374 268.2541 91.8154 15.27575233 00
| Epoch (UTC): | 25 May 2026 12:34:02 |
| Eccentricity: | 0.0001374 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.4387° |
| argument of perigee: | 268.2541° |
| revolutions per day: | 15.27575233 |
| mean anomaly at epoch: | 91.8154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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