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 52472U 26145.08028811 +.00000000 +00000-0 +21623-5 0 00008
2 52472 53.2144 76.1893 0001858 57.5638 302.5534 15.08839646 03
| Epoch (UTC): | 25 May 2026 01:55:36 |
| Eccentricity: | 0.0001858 |
| inclination: | 53.2144° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 76.1893° |
| argument of perigee: | 57.5638° |
| revolutions per day: | 15.08839646 |
| mean anomaly at epoch: | 302.5534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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