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 26139.40797708 +.00000000 +00000-0 +23407-4 0 00000
2 19211 82.5276 32.0013 0021128 166.7531 193.4245 14.85440810 01
| Epoch (UTC): | 19 May 2026 09:47:29 |
| Eccentricity: | 0.0021128 |
| inclination: | 82.5276° |
| perigee height: | 597 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 32.0013° |
| argument of perigee: | 166.7531° |
| revolutions per day: | 14.85440810 |
| mean anomaly at epoch: | 193.4245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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