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 52129U 26145.51729865 +.00000000 +00000-0 +39487-3 0 00007
2 52129 53.2112 84.2283 0001426 87.8069 272.3087 15.08803364 00
| Epoch (UTC): | 25 May 2026 12:24:54 |
| Eccentricity: | 0.0001426 |
| inclination: | 53.2112° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 84.2283° |
| argument of perigee: | 87.8069° |
| revolutions per day: | 15.08803364 |
| mean anomaly at epoch: | 272.3087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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