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 52366U 26145.34800856 +.00000000 +00000-0 +10984-3 0 00002
2 52366 53.2120 204.9881 0001260 82.8509 277.2627 15.08833263 02
| Epoch (UTC): | 25 May 2026 08:21:07 |
| Eccentricity: | 0.0001260 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 204.9881° |
| argument of perigee: | 82.8509° |
| revolutions per day: | 15.08833263 |
| mean anomaly at epoch: | 277.2627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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