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 66041U 26145.42884323 +.00000000 +00000-0 +18438-3 0 00009
2 66041 89.0026 45.4896 0001870 78.4837 281.6524 13.51006382 00
| Epoch (UTC): | 25 May 2026 10:17:32 |
| Eccentricity: | 0.0001870 |
| inclination: | 89.0026° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.4896° |
| argument of perigee: | 78.4837° |
| revolutions per day: | 13.51006382 |
| mean anomaly at epoch: | 281.6524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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