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 55570U 26145.13799847 +.00000000 +00000-0 +64261-5 0 00005
2 55570 43.0055 293.5449 0001738 265.3962 94.6692 15.27576168 03
| Epoch (UTC): | 25 May 2026 03:18:43 |
| Eccentricity: | 0.0001738 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 293.5449° |
| argument of perigee: | 265.3962° |
| revolutions per day: | 15.27576168 |
| mean anomaly at epoch: | 94.6692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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