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 41886U 26145.03942524 +.00000000 +00000-0 +33050-3 0 00001
2 41886 34.9421 17.7391 0008993 331.1630 28.8599 15.62583404 05
| Epoch (UTC): | 25 May 2026 00:56:46 |
| Eccentricity: | 0.0008993 |
| inclination: | 34.9421° |
| perigee height: | 374 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 17.7391° |
| argument of perigee: | 331.1630° |
| revolutions per day: | 15.62583404 |
| mean anomaly at epoch: | 28.8599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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