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 52275U 26145.32224919 +.00000000 +00000-0 -12484-4 0 00008
2 52275 53.2121 125.1038 0001183 60.5598 299.5512 15.08839276 05
| Epoch (UTC): | 25 May 2026 07:44:02 |
| Eccentricity: | 0.0001183 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 125.1038° |
| argument of perigee: | 60.5598° |
| revolutions per day: | 15.08839276 |
| mean anomaly at epoch: | 299.5512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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