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 43573U 26145.50609105 +.00000000 +00000-0 +28530-4 0 00001
2 43573 86.3966 66.1555 0002337 81.7900 278.3561 14.34218909 03
| Epoch (UTC): | 25 May 2026 12:08:46 |
| Eccentricity: | 0.0002337 |
| inclination: | 86.3966° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 66.1555° |
| argument of perigee: | 81.7900° |
| revolutions per day: | 14.34218909 |
| mean anomaly at epoch: | 278.3561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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