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 59867U 26145.44764907 +.00000000 +00000-0 -63202-4 0 00005
2 59867 43.0002 204.6482 0001408 270.0563 90.0128 15.27558723 03
| Epoch (UTC): | 25 May 2026 10:44:36 |
| Eccentricity: | 0.0001408 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.6482° |
| argument of perigee: | 270.0563° |
| revolutions per day: | 15.27558723 |
| mean anomaly at epoch: | 90.0128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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