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 59189U 26145.35922218 +.00000000 +00000-0 -52599-5 0 00001
2 59189 43.0013 19.8393 0001270 264.9428 95.1279 15.27578315 00
| Epoch (UTC): | 25 May 2026 08:37:16 |
| Eccentricity: | 0.0001270 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.8393° |
| argument of perigee: | 264.9428° |
| revolutions per day: | 15.27578315 |
| mean anomaly at epoch: | 95.1279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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