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 52136U 26145.10512197 +.00000000 +00000-0 +49825-4 0 00006
2 52136 53.2144 86.0746 0001429 92.2159 267.8997 15.08844759 02
| Epoch (UTC): | 25 May 2026 02:31:22 |
| Eccentricity: | 0.0001429 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 86.0746° |
| argument of perigee: | 92.2159° |
| revolutions per day: | 15.08844759 |
| mean anomaly at epoch: | 267.8997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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