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 55593U 26145.10458780 +.00000000 +00000-0 +17874-4 0 00002
2 55593 43.0028 293.2939 0001257 276.7627 83.3082 15.27577366 08
| Epoch (UTC): | 25 May 2026 02:30:36 |
| Eccentricity: | 0.0001257 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 293.2939° |
| argument of perigee: | 276.7627° |
| revolutions per day: | 15.27577366 |
| mean anomaly at epoch: | 83.3082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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