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 52563U 26145.27394727 +.00000000 +00000-0 +28687-4 0 00008
2 52563 53.2138 150.3198 0001050 72.9966 287.1141 15.08841617 02
| Epoch (UTC): | 25 May 2026 06:34:29 |
| Eccentricity: | 0.0001050 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 150.3198° |
| argument of perigee: | 72.9966° |
| revolutions per day: | 15.08841617 |
| mean anomaly at epoch: | 287.1141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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