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 25682U 26041.52563691 +.00000000 +00000-0 +11871-3 0 00007
2 25682 97.8602 50.9678 0001696 97.5352 15.5714 14.63786611 01
| Epoch (UTC): | 10 February 2026 12:36:55 |
| Eccentricity: | 0.0001696 |
| inclination: | 97.8602° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 50.9678° |
| argument of perigee: | 97.5352° |
| revolutions per day: | 14.63786611 |
| mean anomaly at epoch: | 15.5714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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