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 53136U 26145.38434652 +.00000000 +00000-0 +39974-4 0 00000
2 53136 53.2133 189.8252 0001013 82.9712 277.1396 15.08840410 02
| Epoch (UTC): | 25 May 2026 09:13:27 |
| Eccentricity: | 0.0001013 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 189.8252° |
| argument of perigee: | 82.9712° |
| revolutions per day: | 15.08840410 |
| mean anomaly at epoch: | 277.1396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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