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 19826U 26053.84478961 +.00000000 +00000-0 +64024-4 0 00002
2 19826 82.9553 7.5623 0029345 205.5626 187.1278 13.72542280 00
| Epoch (UTC): | 22 February 2026 20:16:29 |
| Eccentricity: | 0.0029345 |
| inclination: | 82.9553° |
| perigee height: | 969 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 7.5623° |
| argument of perigee: | 205.5626° |
| revolutions per day: | 13.72542280 |
| mean anomaly at epoch: | 187.1278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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