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 26039.61122898 +.00000000 +00000-0 +12522-3 0 00008
2 25682 97.8602 49.1416 0001663 98.7264 12.2225 14.63784081 00
| Epoch (UTC): | 08 February 2026 14:40:10 |
| Eccentricity: | 0.0001663 |
| inclination: | 97.8602° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 49.1416° |
| argument of perigee: | 98.7264° |
| revolutions per day: | 14.63784081 |
| mean anomaly at epoch: | 12.2225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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