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 59638U 26145.49438007 +.00000000 +00000-0 -25709-4 0 00005
2 59638 43.0026 66.4463 0000951 274.0958 85.9785 15.27584569 01
| Epoch (UTC): | 25 May 2026 11:51:54 |
| Eccentricity: | 0.0000951 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.4463° |
| argument of perigee: | 274.0958° |
| revolutions per day: | 15.27584569 |
| mean anomaly at epoch: | 85.9785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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