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 52625U 26145.36641279 +.00000000 +00000-0 -16019-4 0 00001
2 52625 53.2119 284.9022 0001502 102.0087 258.1073 15.08835614 03
| Epoch (UTC): | 25 May 2026 08:47:38 |
| Eccentricity: | 0.0001502 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 284.9022° |
| argument of perigee: | 102.0087° |
| revolutions per day: | 15.08835614 |
| mean anomaly at epoch: | 258.1073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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