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 52498U 26145.16677144 +.00000000 +00000-0 +28006-3 0 00004
2 52498 53.2138 55.7982 0001345 92.0993 268.0153 15.08817230 03
| Epoch (UTC): | 25 May 2026 04:00:09 |
| Eccentricity: | 0.0001345 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 55.7982° |
| argument of perigee: | 92.0993° |
| revolutions per day: | 15.08817230 |
| mean anomaly at epoch: | 268.0153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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