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 41605U 16040G 25353.51682543 .11453613 24279-5 13983-3 0 9999
2 41605 97.0276 23.8359 0008747 238.4233 121.6219 16.49580729529740
| Epoch (UTC): | 19 December 2025 12:24:13 |
| Eccentricity: | 0.0008747 |
| inclination: | 97.0276° |
| perigee height: | 135 km |
| apogee height: | 146 km |
| right ascension of ascending node: | 23.8359° |
| argument of perigee: | 238.4233° |
| revolutions per day: | 16.49580729 |
| mean anomaly at epoch: | 121.6219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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