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 32258U 26066.44628306 +.00000000 +00000-0 +00000-0 0 00006
2 32258 0.0777 87.4965 0000246 342.3958 213.3942 1.00271987 07
| Epoch (UTC): | 07 March 2026 10:42:38 |
| Eccentricity: | 0.0000246 |
| inclination: | 0.0777° |
| perigee height: | 35786 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 87.4965° |
| argument of perigee: | 342.3958° |
| revolutions per day: | 1.00271987 |
| mean anomaly at epoch: | 213.3942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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