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 26073.29174512 +.00000000 +00000-0 +12018-3 0 00000
2 25682 97.8607 81.2745 0001651 79.9794 290.5014 14.63827510 05
| Epoch (UTC): | 14 March 2026 07:00:06 |
| Eccentricity: | 0.0001651 |
| inclination: | 97.8607° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 81.2745° |
| argument of perigee: | 79.9794° |
| revolutions per day: | 14.63827510 |
| mean anomaly at epoch: | 290.5014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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