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 52844U 26145.44140000 +.00000000 +00000-0 +60578-3 0 00006
2 52844 53.2126 49.5682 0001305 100.8587 259.2552 15.08800184 01
| Epoch (UTC): | 25 May 2026 10:35:36 |
| Eccentricity: | 0.0001305 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 49.5682° |
| argument of perigee: | 100.8587° |
| revolutions per day: | 15.08800184 |
| mean anomaly at epoch: | 259.2552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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