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 58804U 26144.98857872 +.00000000 +00000-0 +11388-3 0 00003
2 58804 43.0037 94.4556 0001577 267.2349 92.8323 15.27577787 03
| Epoch (UTC): | 24 May 2026 23:43:33 |
| Eccentricity: | 0.0001577 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 94.4556° |
| argument of perigee: | 267.2349° |
| revolutions per day: | 15.27577787 |
| mean anomaly at epoch: | 92.8323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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