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 41893U 26145.56448833 +.00000000 +00000-0 +00000-0 0 00007
2 41893 0.0162 336.8693 0001336 91.5108 280.8846 1.00272142 06
| Epoch (UTC): | 25 May 2026 13:32:51 |
| Eccentricity: | 0.0001336 |
| inclination: | 0.0162° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 336.8693° |
| argument of perigee: | 91.5108° |
| revolutions per day: | 1.00272142 |
| mean anomaly at epoch: | 280.8846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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