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 56917U 26145.30807822 +.00000000 +00000-0 +80072-5 0 00001
2 56917 43.0065 358.1775 0001425 264.9223 95.1466 15.27563577 03
| Epoch (UTC): | 25 May 2026 07:23:37 |
| Eccentricity: | 0.0001425 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 358.1775° |
| argument of perigee: | 264.9223° |
| revolutions per day: | 15.27563577 |
| mean anomaly at epoch: | 95.1466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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