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 26065.58563277 +.00000000 +00000-0 +14826-3 0 00002
2 25682 97.8608 73.9216 0001731 84.0156 21.4909 14.63816917 08
| Epoch (UTC): | 06 March 2026 14:03:18 |
| Eccentricity: | 0.0001731 |
| inclination: | 97.8608° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 73.9216° |
| argument of perigee: | 84.0156° |
| revolutions per day: | 14.63816917 |
| mean anomaly at epoch: | 21.4909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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