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 56026U 26145.54707698 +.00000000 +00000-0 -37740-4 0 00002
2 56026 43.0028 330.8528 0000960 261.0334 99.0409 15.27565636 08
| Epoch (UTC): | 25 May 2026 13:07:47 |
| Eccentricity: | 0.0000960 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 330.8528° |
| argument of perigee: | 261.0334° |
| revolutions per day: | 15.27565636 |
| mean anomaly at epoch: | 99.0409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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