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 51468U 26145.11892626 +.00000000 +00000-0 +17843-4 0 00007
2 51468 53.2133 295.9768 0001393 92.9760 267.1392 15.08832784 04
| Epoch (UTC): | 25 May 2026 02:51:15 |
| Eccentricity: | 0.0001393 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 295.9768° |
| argument of perigee: | 92.9760° |
| revolutions per day: | 15.08832784 |
| mean anomaly at epoch: | 267.1392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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