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 58223U 26145.63754929 +.00000000 +00000-0 +99854-5 0 00006
2 58223 43.0038 119.9848 0001041 272.6313 87.4420 15.27574735 01
| Epoch (UTC): | 25 May 2026 15:18:04 |
| Eccentricity: | 0.0001041 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 119.9848° |
| argument of perigee: | 272.6313° |
| revolutions per day: | 15.27574735 |
| mean anomaly at epoch: | 87.4420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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