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 15593U 26065.37064284 +.00000000 +00000-0 +77938-4 0 00007
2 15593 82.5397 160.0783 0009995 318.2220 41.8233 14.86812704 06
| Epoch (UTC): | 06 March 2026 08:53:43 |
| Eccentricity: | 0.0009995 |
| inclination: | 82.5397° |
| perigee height: | 601 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 160.0783° |
| argument of perigee: | 318.2220° |
| revolutions per day: | 14.86812704 |
| mean anomaly at epoch: | 41.8233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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