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 19460U 26142.21098751 +.00000000 +00000-0 +39358-4 0 00003
2 19460 84.9842 128.1749 0003272 154.7739 205.3615 14.34436349 02
| Epoch (UTC): | 22 May 2026 05:03:49 |
| Eccentricity: | 0.0003272 |
| inclination: | 84.9842° |
| perigee height: | 775 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 128.1749° |
| argument of perigee: | 154.7739° |
| revolutions per day: | 14.34436349 |
| mean anomaly at epoch: | 205.3615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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