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 41731U 26025.83936072 +.00000000 +00000-0 +24072-3 0 00000
2 41731 97.2882 320.5748 0008634 239.4939 120.5513 16.48001705 02
| Epoch (UTC): | 25 January 2026 20:08:40 |
| Eccentricity: | 0.0008634 |
| inclination: | 97.2882° |
| perigee height: | 139 km |
| apogee height: | 150 km |
| right ascension of ascending node: | 320.5748° |
| argument of perigee: | 239.4939° |
| revolutions per day: | 16.48001705 |
| mean anomaly at epoch: | 120.5513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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