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 52280U 26145.36273977 +.00000000 +00000-0 +55268-4 0 00002
2 52280 53.2134 124.9198 0001192 82.0318 278.0809 15.08830553 08
| Epoch (UTC): | 25 May 2026 08:42:20 |
| Eccentricity: | 0.0001192 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 124.9198° |
| argument of perigee: | 82.0318° |
| revolutions per day: | 15.08830553 |
| mean anomaly at epoch: | 278.0809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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