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 52348U 26145.60468500 +.00000000 +00000-0 +61629-4 0 00000
2 52348 53.2133 213.8350 0001116 86.2141 273.8979 15.08840966 06
| Epoch (UTC): | 25 May 2026 14:30:44 |
| Eccentricity: | 0.0001116 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 213.8350° |
| argument of perigee: | 86.2141° |
| revolutions per day: | 15.08840966 |
| mean anomaly at epoch: | 273.8979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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