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 59025U 26145.50197655 +.00000000 +00000-0 +43968-4 0 00004
2 59025 43.0025 313.3915 0000366 276.7155 83.3655 15.27569329 09
| Epoch (UTC): | 25 May 2026 12:02:50 |
| Eccentricity: | 0.0000366 |
| inclination: | 43.0025° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 313.3915° |
| argument of perigee: | 276.7155° |
| revolutions per day: | 15.27569329 |
| mean anomaly at epoch: | 83.3655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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