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 19223U 26053.78952006 +.00000000 +00000-0 +53076-4 0 00008
2 19223 89.9786 78.1535 0030690 171.5347 9.5473 13.22945631 05
| Epoch (UTC): | 22 February 2026 18:56:54 |
| Eccentricity: | 0.0030690 |
| inclination: | 89.9786° |
| perigee height: | 1150 km |
| apogee height: | 1197 km |
| right ascension of ascending node: | 78.1535° |
| argument of perigee: | 171.5347° |
| revolutions per day: | 13.22945631 |
| mean anomaly at epoch: | 9.5473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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