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 58232U 26145.48509352 +.00000000 +00000-0 -44985-3 0 00001
2 58232 43.0020 211.1763 0001187 271.7722 88.2994 15.27510968 01
| Epoch (UTC): | 25 May 2026 11:38:32 |
| Eccentricity: | 0.0001187 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.1763° |
| argument of perigee: | 271.7722° |
| revolutions per day: | 15.27510968 |
| mean anomaly at epoch: | 88.2994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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