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 52841U 26145.03658728 +.00000000 +00000-0 -24560-4 0 00002
2 52841 53.2132 51.3837 0001487 80.0374 280.0786 15.08844094 01
| Epoch (UTC): | 25 May 2026 00:52:41 |
| Eccentricity: | 0.0001487 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 51.3837° |
| argument of perigee: | 80.0374° |
| revolutions per day: | 15.08844094 |
| mean anomaly at epoch: | 280.0786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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