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 06324U 26071.74966814 +.00000000 +00000-0 +98681-4 0 00005
2 06324 74.0767 308.5592 0008762 339.1258 20.9541 14.45282134 09
| Epoch (UTC): | 12 March 2026 17:59:31 |
| Eccentricity: | 0.0008762 |
| inclination: | 74.0767° |
| perigee height: | 735 km |
| apogee height: | 747 km |
| right ascension of ascending node: | 308.5592° |
| argument of perigee: | 339.1258° |
| revolutions per day: | 14.45282134 |
| mean anomaly at epoch: | 20.9541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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