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 41924U 26145.49975088 +.00000000 +00000-0 -93272-5 0 00000
2 41924 86.3965 66.2451 0002045 85.0493 275.0936 14.34217435 09
| Epoch (UTC): | 25 May 2026 11:59:38 |
| Eccentricity: | 0.0002045 |
| inclination: | 86.3965° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 66.2451° |
| argument of perigee: | 85.0493° |
| revolutions per day: | 14.34217435 |
| mean anomaly at epoch: | 275.0936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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