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 59517U 26145.56439391 +.00000000 +00000-0 +20421-4 0 00001
2 59517 43.0049 243.7896 0000936 256.5192 103.5556 15.27587880 02
| Epoch (UTC): | 25 May 2026 13:32:43 |
| Eccentricity: | 0.0000936 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 243.7896° |
| argument of perigee: | 256.5192° |
| revolutions per day: | 15.27587880 |
| mean anomaly at epoch: | 103.5556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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