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 52862U 26145.11478509 +.00000000 +00000-0 +37202-4 0 00007
2 52862 53.2128 41.0317 0001319 119.1236 240.9888 15.08836399 00
| Epoch (UTC): | 25 May 2026 02:45:17 |
| Eccentricity: | 0.0001319 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 41.0317° |
| argument of perigee: | 119.1236° |
| revolutions per day: | 15.08836399 |
| mean anomaly at epoch: | 240.9888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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