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 52541U 26145.22611168 +.00000000 +00000-0 +28240-3 0 00004
2 52541 53.2123 150.5336 0000974 73.9274 286.1826 15.08825679 04
| Epoch (UTC): | 25 May 2026 05:25:36 |
| Eccentricity: | 0.0000974 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 150.5336° |
| argument of perigee: | 73.9274° |
| revolutions per day: | 15.08825679 |
| mean anomaly at epoch: | 286.1826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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