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 19468U 26137.42091653 +.00000000 +00000-0 +18174-3 0 00004
2 19468 98.9602 186.5272 0071352 17.6348 353.1127 14.03766647 08
| Epoch (UTC): | 17 May 2026 10:06:07 |
| Eccentricity: | 0.0071352 |
| inclination: | 98.9602° |
| perigee height: | 829 km |
| apogee height: | 933 km |
| right ascension of ascending node: | 186.5272° |
| argument of perigee: | 17.6348° |
| revolutions per day: | 14.03766647 |
| mean anomaly at epoch: | 353.1127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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