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 41581U 26144.56676985 +.00000000 +00000-0 +00000-0 0 00001
2 41581 0.0128 255.2233 0001210 17.5633 78.3655 1.00273589 02
| Epoch (UTC): | 24 May 2026 13:36:08 |
| Eccentricity: | 0.0001210 |
| inclination: | 0.0128° |
| perigee height: | 35781 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 255.2233° |
| argument of perigee: | 17.5633° |
| revolutions per day: | 1.00273589 |
| mean anomaly at epoch: | 78.3655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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