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 53426U 26145.34296663 +.00000000 +00000-0 +21789-3 0 00000
2 53426 53.2122 120.1639 0001314 97.5846 262.5296 15.08825839 08
| Epoch (UTC): | 25 May 2026 08:13:52 |
| Eccentricity: | 0.0001314 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 120.1639° |
| argument of perigee: | 97.5846° |
| revolutions per day: | 15.08825839 |
| mean anomaly at epoch: | 262.5296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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