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 21891U 26040.11833934 +.00000000 +00000-0 +26276-3 0 00004
2 21891 19.9962 312.2719 0038277 334.6674 25.1872 14.93238292 02
| Epoch (UTC): | 09 February 2026 02:50:24 |
| Eccentricity: | 0.0038277 |
| inclination: | 19.9962° |
| perigee height: | 561 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 312.2719° |
| argument of perigee: | 334.6674° |
| revolutions per day: | 14.93238292 |
| mean anomaly at epoch: | 25.1872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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