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 52001U 26145.40140659 +.00000000 +00000-0 +14685-3 0 00005
2 52001 53.2130 34.7577 0001219 86.7298 273.3834 15.08833449 05
| Epoch (UTC): | 25 May 2026 09:38:01 |
| Eccentricity: | 0.0001219 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.7577° |
| argument of perigee: | 86.7298° |
| revolutions per day: | 15.08833449 |
| mean anomaly at epoch: | 273.3834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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