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 52566U 26145.31075250 +.00000000 +00000-0 +33758-3 0 00007
2 52566 53.2115 150.1549 0001089 81.1635 278.9480 15.08807790 03
| Epoch (UTC): | 25 May 2026 07:27:29 |
| Eccentricity: | 0.0001089 |
| inclination: | 53.2115° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 150.1549° |
| argument of perigee: | 81.1635° |
| revolutions per day: | 15.08807790 |
| mean anomaly at epoch: | 278.9480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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