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 52133U 26145.10880657 +.00000000 +00000-0 +24935-6 0 00009
2 52133 53.2164 86.0599 0001454 87.1558 272.9600 15.08841036 04
| Epoch (UTC): | 25 May 2026 02:36:40 |
| Eccentricity: | 0.0001454 |
| inclination: | 53.2164° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 86.0599° |
| argument of perigee: | 87.1558° |
| revolutions per day: | 15.08841036 |
| mean anomaly at epoch: | 272.9600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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