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 52361U 26145.37652839 +.00000000 +00000-0 +39927-4 0 00005
2 52361 53.2127 214.8631 0001149 86.3089 273.8035 15.08838848 04
| Epoch (UTC): | 25 May 2026 09:02:12 |
| Eccentricity: | 0.0001149 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 214.8631° |
| argument of perigee: | 86.3089° |
| revolutions per day: | 15.08838848 |
| mean anomaly at epoch: | 273.8035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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