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 26067.96376097 +.00000000 +00000-0 +14449-3 0 00009
2 25682 97.8609 76.1907 0001709 82.9345 307.1789 14.63820431 09
| Epoch (UTC): | 08 March 2026 23:07:48 |
| Eccentricity: | 0.0001709 |
| inclination: | 97.8609° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 76.1907° |
| argument of perigee: | 82.9345° |
| revolutions per day: | 14.63820431 |
| mean anomaly at epoch: | 307.1789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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