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 19419U 26134.15858838 +.00000000 +00000-0 +11319-3 0 00007
2 19419 90.0440 20.8256 0096142 170.3003 303.7891 13.42653049 00
| Epoch (UTC): | 14 May 2026 03:48:22 |
| Eccentricity: | 0.0096142 |
| inclination: | 90.0440° |
| perigee height: | 1028 km |
| apogee height: | 1171 km |
| right ascension of ascending node: | 20.8256° |
| argument of perigee: | 170.3003° |
| revolutions per day: | 13.42653049 |
| mean anomaly at epoch: | 303.7891° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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