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 59486U 26144.69750689 +.00000000 +00000-0 -31641-4 0 00002
2 59486 43.0020 270.1798 0001161 287.0593 73.0132 15.27575142 05
| Epoch (UTC): | 24 May 2026 16:44:24 |
| Eccentricity: | 0.0001161 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.1798° |
| argument of perigee: | 287.0593° |
| revolutions per day: | 15.27575142 |
| mean anomaly at epoch: | 73.0132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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