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 26075.27424001 +.00000000 +00000-0 +10782-3 0 00007
2 25682 97.8607 83.1661 0001626 79.2356 292.2897 14.63829767 06
| Epoch (UTC): | 16 March 2026 06:34:54 |
| Eccentricity: | 0.0001626 |
| inclination: | 97.8607° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 83.1661° |
| argument of perigee: | 79.2356° |
| revolutions per day: | 14.63829767 |
| mean anomaly at epoch: | 292.2897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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