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 59731U 26145.39139736 +.00000000 +00000-0 +28245-4 0 00002
2 59731 43.0003 110.0712 0000784 271.9867 88.0894 15.27583939 07
| Epoch (UTC): | 25 May 2026 09:23:36 |
| Eccentricity: | 0.0000784 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.0712° |
| argument of perigee: | 271.9867° |
| revolutions per day: | 15.27583939 |
| mean anomaly at epoch: | 88.0894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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