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 52456U 26145.53664992 +.00000000 +00000-0 +10332-3 0 00009
2 52456 53.2123 84.1411 0001420 87.1858 272.9297 15.08830881 03
| Epoch (UTC): | 25 May 2026 12:52:46 |
| Eccentricity: | 0.0001420 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 84.1411° |
| argument of perigee: | 87.1858° |
| revolutions per day: | 15.08830881 |
| mean anomaly at epoch: | 272.9297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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