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 41744U 26144.36776939 +.00000000 +00000-0 +00000-0 0 00000
2 41744 4.1376 77.4847 0008631 334.8808 145.8544 1.00279232 09
| Epoch (UTC): | 24 May 2026 08:49:35 |
| Eccentricity: | 0.0008631 |
| inclination: | 4.1376° |
| perigee height: | 35748 km |
| apogee height: | 35821 km |
| right ascension of ascending node: | 77.4847° |
| argument of perigee: | 334.8808° |
| revolutions per day: | 1.00279232 |
| mean anomaly at epoch: | 145.8544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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