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 41771U 26145.32257161 +.00000000 +00000-0 +30518-3 0 00008
2 41771 96.9191 168.0633 0001927 66.6079 293.5375 15.47777027 08
| Epoch (UTC): | 25 May 2026 07:44:30 |
| Eccentricity: | 0.0001927 |
| inclination: | 96.9191° |
| perigee height: | 422 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 168.0633° |
| argument of perigee: | 66.6079° |
| revolutions per day: | 15.47777027 |
| mean anomaly at epoch: | 293.5375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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