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 52996U 26145.16453881 +.00000000 +00000-0 +55888-4 0 00006
2 52996 53.2126 111.0943 0001186 80.0277 280.0849 15.08839980 03
| Epoch (UTC): | 25 May 2026 03:56:56 |
| Eccentricity: | 0.0001186 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 111.0943° |
| argument of perigee: | 80.0277° |
| revolutions per day: | 15.08839980 |
| mean anomaly at epoch: | 280.0849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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