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 52561U 26145.27026736 +.00000000 +00000-0 +26472-4 0 00008
2 52561 53.2140 150.3379 0001112 72.2306 287.8807 15.08839946 02
| Epoch (UTC): | 25 May 2026 06:29:11 |
| Eccentricity: | 0.0001112 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 150.3379° |
| argument of perigee: | 72.2306° |
| revolutions per day: | 15.08839946 |
| mean anomaly at epoch: | 287.8807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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