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 52335U 26145.41240823 +.00000000 +00000-0 +58507-4 0 00002
2 52335 53.2139 224.7011 0001132 86.9457 273.1664 15.08838329 02
| Epoch (UTC): | 25 May 2026 09:53:52 |
| Eccentricity: | 0.0001132 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 224.7011° |
| argument of perigee: | 86.9457° |
| revolutions per day: | 15.08838329 |
| mean anomaly at epoch: | 273.1664° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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