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 26040.24888016 +.00000000 +00000-0 +66695-4 0 00002
2 19211 82.5271 125.1173 0021984 136.0886 224.2082 14.85354621 06
| Epoch (UTC): | 09 February 2026 05:58:23 |
| Eccentricity: | 0.0021984 |
| inclination: | 82.5271° |
| perigee height: | 597 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 125.1173° |
| argument of perigee: | 136.0886° |
| revolutions per day: | 14.85354621 |
| mean anomaly at epoch: | 224.2082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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