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 58228U 26145.36444257 +.00000000 +00000-0 +16366-4 0 00007
2 58228 43.0039 121.3804 0001207 273.4296 86.6418 15.27574077 06
| Epoch (UTC): | 25 May 2026 08:44:47 |
| Eccentricity: | 0.0001207 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.3804° |
| argument of perigee: | 273.4296° |
| revolutions per day: | 15.27574077 |
| mean anomaly at epoch: | 86.6418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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