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 06256U 26088.11417516 +.00000000 +00000-0 +22687-4 0 00001
2 06256 81.2720 230.4629 0028773 5.2224 354.9241 14.09469846 08
| Epoch (UTC): | 29 March 2026 02:44:24 |
| Eccentricity: | 0.0028773 |
| inclination: | 81.2720° |
| perigee height: | 840 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 230.4629° |
| argument of perigee: | 5.2224° |
| revolutions per day: | 14.09469846 |
| mean anomaly at epoch: | 354.9241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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