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 55596U 26145.44951447 +.00000000 +00000-0 -11132-4 0 00002
2 55596 43.0034 291.5801 0001126 272.1385 87.9338 15.27574312 05
| Epoch (UTC): | 25 May 2026 10:47:18 |
| Eccentricity: | 0.0001126 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.5801° |
| argument of perigee: | 272.1385° |
| revolutions per day: | 15.27574312 |
| mean anomaly at epoch: | 87.9338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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