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 19211U 26039.30575875 +.00000000 +00000-0 +70670-4 0 00001
2 19211 82.5272 126.0026 0021930 139.0723 221.2144 14.85353548 01
| Epoch (UTC): | 08 February 2026 07:20:17 |
| Eccentricity: | 0.0021930 |
| inclination: | 82.5272° |
| perigee height: | 597 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 126.0026° |
| argument of perigee: | 139.0723° |
| revolutions per day: | 14.85353548 |
| mean anomaly at epoch: | 221.2144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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