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 26039.19286060 +.00000000 +00000-0 +13146-3 0 00006
2 25682 97.8602 48.7425 0001656 99.0318 328.5982 14.63783608 08
| Epoch (UTC): | 08 February 2026 04:37:43 |
| Eccentricity: | 0.0001656 |
| inclination: | 97.8602° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 48.7425° |
| argument of perigee: | 99.0318° |
| revolutions per day: | 14.63783608 |
| mean anomaly at epoch: | 328.5982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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