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 52873U 26145.06418854 +.00000000 +00000-0 +11463-3 0 00000
2 52873 53.2129 31.2626 0001848 87.9771 272.1433 15.08835329 05
| Epoch (UTC): | 25 May 2026 01:32:25 |
| Eccentricity: | 0.0001848 |
| inclination: | 53.2129° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 31.2626° |
| argument of perigee: | 87.9771° |
| revolutions per day: | 15.08835329 |
| mean anomaly at epoch: | 272.1433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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