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 52636U 26145.41056574 +.00000000 +00000-0 +54088-4 0 00004
2 52636 53.2139 284.7066 0001215 90.0258 270.0873 15.08837988 07
| Epoch (UTC): | 25 May 2026 09:51:12 |
| Eccentricity: | 0.0001215 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 284.7066° |
| argument of perigee: | 90.0258° |
| revolutions per day: | 15.08837988 |
| mean anomaly at epoch: | 270.0873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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